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Concise Eurocode 2 for Bridges
A cement and concrete industry publication
For the design of concrete bridges to BS EN 1992-1-1 and BS EN 1992-2 and their National Annexes
O Brooker BEng CEng MICE MIStructE
P A Jackson BSc(Hons) PhD CEng FICE FIStructE
S W Salim BEng(Hons) PhD CEng MICE
ForewordThe introduction of European standards to UK construction is a significant event as for the first time all design and construction codes within the EU will be harmonised. The ten design standards, known as the Eurocodes, will affect all design and construction activities as current British Standards for structural design are due to be withdrawn in March 2010.
The cement and concrete industry recognised the need to enable UK design professionals to use Eurocode 2, Design of concrete structures, quickly efficiently and with confidence. Supported by government, consultants and relevant industry bodies, the Concrete Industry Eurocode 2 Group (CIEG) was formed in 1999 and this group has provided the guidance for a coordinated and collaborative approach to the introduction of Eurocode 2.
As a result, a range of resources is being developed and made available through The Concrete Centre (see www.eurocode2.info). One of those resources, Concise Eurocode 2, published in 2006, is targeted at structural engineers designing concrete framed buildings. Whilst there are many similarities in the design of buildings and bridges, there are also significant differences and hence Eurocode 2 has a distinct part for the design of bridges. This publication is based on the style of Concise Eurocode 2, but has been completely revised and rewritten to suit the requirements of Eurocode 2, Part 2 and the current design practices for concrete bridge design.
Relevant extracts have been incorporated from Precast Eurocode 2: Design manual published by British Precast, which is a similar document for designers of precast concrete. The authors are grateful for the permission granted by British Precast.
AcknowledgementsThe Concrete Centre would to thank Neil Loudon and Hideo Takano, both of the Highways Agency, for their support and comments in producing this document. We would also like to thank Steve Denton of Parsons Brinckerhoff, Chris Hendy of Atkins and Paul White of Halcrow for their helpful comments. Thanks are also due to Gillian Bond, Sally Huish and the design team at Michael Burbridge Ltd for their work on the production.
The copyright of British Standards extracts reproduced in this document is held by the British Standards Institution (BSI). Extracts have been reproduced with BSI’s permission under the terms of Licence No: 2009RM0003. No other use of this material is permitted. This publication is not intended to be a replacement for the standard and may not reflect the most up-to-date status of the standard. British Standards can be obtained in PDF or hard copy formats from the BSI online shop: www.bsigroup.com/Shop or by contacting BSI Customer Services for hard copies only: Tel:+44 (0)20 8996 9001, Email: [email protected].
Published by The Concrete Centre, part of the Mineral Products Association Riverside House, 4 Meadows Business Park, Station Approach, Blackwater, Camberley, Surrey GU17 9AB Tel: +44 (0)1276 606800 Fax: +44 (0)1276 606801 www.concretecentre.com
Cement and Concrete Industry Publications (CCIP) are produced through an industry initiative to publish technical guidance in support of concrete design and construction.
CCIP publications are available from the Concrete Bookshop at www.concretebookshop.com Tel: +44 (0)7004 607777
CCIP-038Published July 2009ISBN 978-1-904818-82-3Price Group P© MPA – The Concrete Centre
All advice or information from MPA - The Concrete Centre is intended only for use in the UK by those who will evaluate the significance and limitations of its contents and take responsibility for its use and application. No liability (including that for negligence) for any loss resulting from such advice or information is accepted by Mineral Products Association or its subcontractors, suppliers or advisors. Readers should note that the publications from MPA - The Concrete Centre are subject to revision from time to time and should therefore ensure that they are in possession of the latest version.
Printed by Michael Burbridge Ltd, Maidenhead, UK.
i
Symbols iv
1 Introduction 1
1.1 Scope 2
2 Basis of design 3
2.1 General 3
2.2 Basicrequirements 3
2.3 Limitstatedesign 4
2.4 Assumptions 9
2.5 Foundationdesign 10
3 Materials 11
3.1 Concrete 11
3.2 Steelreinforcement 13
3.3 Prestressingsteel 14
4 Durability and cover 17
4.1 General 17
4.2 Coverforbond,cmin,b 18
4.3 Coverfordurability,cmin,dur 18
4.4 Chemicalattack 22
4.5 Dcdevandotherallowances 23
5 Structural analysis 25
5.1 General 25
5.2 Idealisationofthestructure 25
5.3 Methodsofanalysis 27
5.4 Loading 29
5.5 Geometricalimperfections 29
5.6 Designmomentsincolumns 31
5.7 Corbels 36
5.8 Lateralinstabilityofslenderbeams 38
6 Bending and axial force 39
6.1 Assumptions 39
7 Shear 41
7.1 General 41
7.2 Resistanceofmembersnotrequiringshearreinforcement 41
7.3 Resistanceofmembersrequiringshearreinforcement 44
Contents
ConciseEurocode2forBridges
ii
8 Punching shear 50
8.1 General 50
8.2 Appliedshearstress 50
8.3 Controlperimeters 54
8.4 Punchingshearresistancewithoutshearreinforcement 55
8.5 Punchingshearresistancewithshearreinforcement 56
8.6 Punchingshearresistanceadjacenttocolumns 56
8.7 Controlperimeterwhereshearreinforcementisnolongerrequired,uout 56
8.8 Distributionofshearreinforcement 57
8.9 Punchingshearresistanceoffoundationbases 58
9 Torsion 59
9.1 General 59
9.2 Torsionalresistances 59
9.3 Combinedtorsionandshear 61
10 Strut-and-tie models, bearing zones and partially loaded areas 62
10.1 Designwithstrut-and-tiemodels 62
10.2 Partiallyloadedareas 65
10.3 Bearingzonesofbridges 66
11 Prestressed members and structures 67
11.1 General 67
11.2 BrittleFracture 67
11.3 Prestressingforceduringtensioning 69
12 Fatigue 72
12.1 Verificationconditions 72
12.2 Internalforcesandstressesforfatigueverification 72
12.3 Verificationofconcreteundercompressionorshear 73
12.4 Limitingstressrangeforreinforcementundertension 74
13 Serviceability 76
13.1 General 76
13.2 StressLimitation 76
13.3 Calculationofcrackwidths 76
13.4 Controlofcracking 79
13.5 Minimumreinforcementareasofmainbars 80
13.6 Controlofdeflection 83
14 Detailing – general requirements 85
14.1 General 85
14.2 Spacingofbars 85
14.3 Mandrelsizesforbentbars 85
14.4 Anchorageofbars 86
14.5 Ultimatebondstress 88
14.6 AnchorageoftendonsatULS 89
14.7 Anchorageoftendonsattransferofprestress 90
14.8 Laps 90
iii
15 Detailing – particular requirements 94
15.1 General 94
15.2 Beams 94
15.3 One-wayandtwo-wayspanningslabs 98
15.4 Flatslabs 98
15.5 Columns 100
15.6 Walls 101
15.7 Pilecaps 102
15.8 Boredpiles 103
15.9 Requirementsforvoidedslabs 103
15.10 Prestressing 104
15.11 Connections 105
15.12 Bearings 106
16 Design for the execution stages 109
17 Design aids 110
17.1 Designforbending 110
17.2 Designforbeamshear 112
17.3 Designforpunchingshear 114
17.4 Designforaxialloadandbending 115
18 References 122
iv
Symbols and abbreviations used in this publication
Symbol Definition
IxI Absolutevalueofx
1/r Curvatureataparticularsection
A Cross-sectionalarea;Accidentalaction
A, B, C Variablesusedinthedeterminationofllim
Ac Cross-sectionalareaofconcrete
Ac,eff Effectiveareaofconcreteintension
Act Areaofconcreteinthatpartofthesectionthatiscalculatedtobeintensionjustbeforetheformationofthefirstcrack
Ad Designvalueofanaccidentalaction
Ak Areaenclosedbythecentrelinesofconnectingwallsincludingtheinnerhollowarea(torsion)
Ap Areaofprestressingtendonortendons
Ap' AreaofprestressingtendonswithinAc,eff
As Cross-sectionalareaofreinforcement
As,min Minimumcross-sectionalareaofreinforcement
As,prov Areaofsteelprovided
As,req Areaofsteelrequired
As1 Areaofreinforcingsteelinlayer1
As2 Areaofcompressionsteel(inlayer2)
Asl Areaofthetensilereinforcementextendingatleastlbd+dbeyondthesectionconsidered
AsM(AsN) Totalareaofreinforcementrequiredinsymmetrical,rectangularcolumnstoresistmoment(axialload)usingsimplifiedcalculationmethod
Ast Cross-sectionalareaoftransversesteel(atlaps)
Asw Cross-sectionalareaofshearreinforcement
Asw Areaofpunchingshearreinforcementinoneperimeteraroundthecolumn
Asw,min Minimumcross-sectionalareaofshearreinforcement
Asw,min Minimumareaofpunchingshearreinforcementinoneperimeteraroundthecolumn
a Distance,allowanceatsupports
a Geometricdata
Da Deviationforgeometricaldata
a Anexponent(inconsideringbiaxialbendingofcolumns)
a Projectionofthefootingfromthefaceofthecolumnorwall
ab Halfthecentre-to-centrespacingofbars(perpendiculartotheplaneofthebend)
al Distancebywhichthelocationwhereabarisnolongerrequiredforbendingmomentisdisplacedtoallowfortheforcesfromthetrussmodelforshear.(‘Shift’distanceforcurtailment)
av Distancebetweenbearingsorfaceofsupportandfaceofload
a1,b1 Dimensionsofthecontrolperimeteraroundanelongatedsupport(punchingshear)
b Overallwidthofacross-section,orflangewidthinaT-orL-beam
b0 Widthofthebottomflangeofthesection
be Effectivewidthofaflatslab(adjacenttoperimetercolumn)
beff Effectivewidthofaflange
beq(heq) Equivalentwidth(height)ofcolumn=b(h)forrectangularsections
bmin MinimumwidthofwebonT-,I-orL-beams
bt Meanwidthofthetensionzone.ForaT-beamwiththeflangeincompression,onlythewidthofthewebistakenintoaccount
v
Symbol Definition
bw WidthofthewebonT-,I-orL-beams.Minimumwidthbetweentensionandcompressionchords
by,bz Dimensionsofthecontrolperimeter(punchingshear)
Dc Permitteddeviationfromcnom(BSEN13760)
Dc,dev Allowancemadeindesignfordeviation
cmin Minimumcover(duetotherequirementsforbond,cmin,bordurabilitycmin,dur)
cnom Nominalcover(minimumcoverplusallowancefordeviations)
cy,cx Columndimensionsinplan
c1,c2 Dimensionsofarectangularcolumn.Foredgecolumns,c1ismeasuredperpendiculartothefreeedge(punchingshear)
D Diameterofacircularcolumn;Diameterofmandrel;Diameter
DEd Fatiguedamagefactor
d Effectivedepthtotensionsteel
d2 Effectivedepthtocompressionsteel
dc Effectivedepthofconcreteincompression
deff Effectivedepthoftheslabtakenastheaverageoftheeffectivedepthsintwoorthogonaldirections(punchingshear)
dg Largestmaximumaggregatesize
dl Ashortlengthofaperimeter(punchingshear)
E Effectofaction;Elasticmodulus
Ec,Ec(t) Tangentmodulusofelasticityofnormalweightconcreteatastressofsc=0andattime,t,days
Ec,eff Effectivemodulusofelasticityofconcrete
Ecd Designvalueofmodulusofelasticityofconcrete
Ecm Secantmodulusofelasticityofconcrete
Ed Designvalueoftheeffectofactions
EI Bendingstiffness
Ep Designvalueofelasticityofprestressingsteel
Es Designvalueofmodulusofelasticityofreinforcingsteel
Exp. Expression
EQU Staticequilibrium
e Eccentricity
e2 Deflection(usedinassessingM2inslendercolumns)
ei Eccentricityduetoimperfections
epar Eccentricityparalleltotheslabedgeresultingfromamomentaboutanaxisperpendiculartotheslabedge(punchingshear)
ey,ez Eccentricity,MEd/VEdalongyandzaxesrespectively(punchingshear)
F Action
Fbt Tensileforceinthebaratthestartofthebendcausedbyultimateloads
Fc(Fs) Forceinconcrete(steel)
Fcd Designvalueoftheconcretecompressionforceinthedirectionofthelongitudinalmemberaxis
Fcr Absolutevalueofthetensileforcewithintheflangeimmediatelypriortocrackingduetothecrackingmomentcalculatedwithfct,eff
Fd Designvalueofanaction
FE Tensileforceinreinforcementtobeanchored
FEd Compressiveforce,designvalueofsupportreaction
Fk Characteristicvalueofanaction
Symbols and abbreviations used in this publication
vi
Symbol Definition
Frep Representativeaction(=c Fkwherec=factortoconvertcharacteristictorepresentativeaction)
FRs Resistingtensileforceinsteel
Fs Tensileforceinthebar
Ftd Designvalueofthetensileforceinlongitudinalreinforcement
DFtd Additionaltensileforceinlongitudinalreinforcementduetothetrussshearmodel
Fwd Designshearstrengthofweld,designvalueoftheforceinstirrupsincorbels
FWk Characteristicvalueofwindforce(AnnexA2,BSEN1990)
f Frequency
fbd Ultimatebondstress
fc Compressivestrengthofconcrete
fcd Designvalueofconcretecompressivestrength
fcd,fat Designfatiguestrengthofconcrete
fcd,pl Designcompressivestrengthofplainconcrete
fck Characteristiccompressivecylinderstrengthofconcreteat28days
fck(t0) Characteristicconcretecompressivestrengthattimeofloading
fck,cube Characteristiccompressivecubestrengthofconcreteat28days
fcm Meanvalueofconcretecylindercompressivestrength
fct,d Designtensilestrengthofconcrete(actfct,k/gC)
fct,eff Meantensilestrengthofconcreteeffectiveatthetimecracksmaybefirstexpectedtooccur.fct,eff=fctmattheappropriateage
fct,k Characteristicaxialtensilestrengthofconcrete
fctb Tensilestrengthpriortocrackinginbiaxialstateofstress
fctm Meanvalueofaxialtensilestrengthofconcrete
fctx Appropriatetensilestrengthforevaluationofcrackingbendingmoment
fctk,0.05 5%fractilevalueofaxialtensilestrengthofconcrete
fctk,0.95 95%fractilevalueofaxialtensilestrengthofconcrete
fcvd Concretedesignstrengthinshearandcompression(plainconcrete)
fp Tensilestrengthofprestressingsteel
fp0.1 0.1%proof-stressofprestressingsteel
fp0.1k Characteristic0.1%proof-stressofprestressingsteel
fp0.2k Characteristic0.2%proof-stressofprestressingsteel
fpk Characteristictensilestrengthofprestressingsteel
fsc CompressivestressincompressionreinforcementatULS
ft Tensilestrengthofreinforcement
ft,k Characteristictensilestrengthofreinforcement
fy Yieldstrengthofreinforcement
fyd Designyieldstrengthoflongitudinalreinforcement,Asl
fyk Characteristicyieldstrengthofreinforcement
fywd Designyieldstrengthoftheshearreinforcement
fywd,ef Effectivedesignstrengthofpunchingshearreinforcement
fywk Characteristicyieldstrengthofshearreinforcement
Gk Characteristicvalueofapermanentaction
gk Characteristicvalueofapermanentactionperunitlengthorarea
Hi Horizontalactionappliedatalevel
h Overalldepthofacross-section;Height
vii
Symbol Definition
h0 Notionalsizeofcross-section
hf Depthoffooting;Thicknessofflange
hH Verticalheightofadroporcolumnheadbelowsoffitofaslab(punchingshear)
hs Depthofslab
I Secondmomentofareaofconcretesection
i Radiusofgyration
J Creepfunction
K MEd/bd2fck.Ameasureoftherelativecompressivestressinamemberinflexure
K Factortoaccountforstructuralsystem(deflection)
K' ValueofKabovewhichcompressionreinforcementisrequired
Kc Factorforcrackingandcreepeffects
Kr Correctionfactorforcurvaturedependingonaxialload
Ks Factorforreinforcementcontribution
Kh Factorfortakingaccountofcreep
k Coefficientorfactor
k Unintentionalangulardisplacementforinternaltendons
kc Coefficientallowingforthenatureofthestressdistributionwithinthesectionimmediatelypriortocrackingandforthechangeoftheleverarmasaresultofcracking(minimumareas)
kt Factorincrackwidthcalculationswhichdependsonthedurationofloading
l Clearheightofcolumnbetweenendrestraints
l Heightofthestructureinmetres
l(orL) Length;Span
l0 Effectivelength(ofcolumns)
l0 Distancebetweenpointsofzeromoment
l0 Designlaplength
lbd Designanchoragelength
lb,eq Equivalentanchoragelength
lb,min Minimumanchoragelength
lb,rqd Basicanchoragelength
leff Effectivespan
lH Horizontaldistancefromcolumnfacetoedgeofadroporcolumnheadbelowsoffitofaslab(punchingshear)
ln Cleardistancebetweenthefacesofsupports
ls Floortoceilingheight
lx,ly Spansofatwo-wayslabinthexandydirections
M Bendingmoment.Momentfromfirstorderanalysis
M' Momentresistanceofasinglyreinforcedsection(abovewhichcompressionreinforcementisrequired)
M0,Eqp Firstorderbendingmomentinquasi-permanentloadcombination(SLS)
M01,M02 FirstorderendmomentsatULSincludingallowancesforimperfections
M0Ed Equivalentfirstordermomentincludingtheeffectofimperfections(ataboutmidheight)
M2 Nominalsecondordermomentinslendercolumns
MEd Designvalueoftheappliedinternalbendingmoment
MEdy,MEdz Designmomentintherespectivedirection
Mfreq Appliedbendingmomentduetofrequentcombination
MRdy,MRdz Momentresistanceintherespectivedirection
viii
Symbol Definition
MRd,max Maximumtransversemomentresistance
Mrep Crackingbendingmoment
m Numberofverticalmemberscontributingtoaneffect
m Mass;Slabcomponents
N Axialforce
NA NationalAnnex
Na,Nb LongitudinalforcescontributingtoHi
NEd Designvalueofaxialforce(tensionorcompression)atULS
NDP NationallyDeterminedParameter(s)aspublishedinacountry’sNationalAnnex
n AxialstressatULS
n Ultimateaction(load)perunitlength(orarea)
n Platecomponents
n Numberofbars
nb Numberofbarsinthebundle
P Prestressingforce
P0 Initialforceattheactiveendofthetendonimmediatelyafterstressing
Qc Characteristicconstructionload
Qfat Characteristicfatigueload
Qk Characteristicvalueofavariableaction
Qk1(Qki) Characteristicvalueofaleadingvariableaction(Characteristicvalueofanaccompanyingvariableaction)
QSn,k Characteristicvalueofsnowload
qk Characteristicvalueofavariableactionperunitlengthorarea
qud Maximumvalueofcombinationreachedinnon-linearanalysis
R Resistance
R/A' Verticalbearingresistanceperunitarea(foundations)
Rd Designvalueoftheresistancetoanaction
RH Relativehumidity
r Radius;Correctingfactorforprestress
rcont Thedistancefromthecentroidofacolumntothecontrolsectionoutsidethecolumnhead
rinf,rsup Allowanceinserviceabilityandfatiguecalculationsforpossiblevariationsinprestress
rm RatiooffirstorderendmomentsincolumnsatULS
S Internalforcesandmoments;Firstmomentofarea
S,N,R Cementtypes
SLS Serviceabilitylimitstate(s)–correspondingtoconditionsbeyondwhichspecifiedservicerequirementsarenolongermet
s Spacingofthestirrups;Spacingbetweencracks
sr Radialspacingofperimetersofshearreinforcement
sr,max Maximumfinalcrackspacing
st Tangentialspacingshearreinforcementalongperimetersofshearreinforcement
T Torsionalmoment;Tensileforce
TEd Designvalueoftheappliedtorsionalmoment
Tk Characteristicvalueofthermalactions
TRd Designtorsionalresistancemoment
TRd,max Maximumdesigntorsionalresistancemomentresistance
t Thickness;Timebeingconsidered;Breadthofsupport;Timeaftertensioning
ix
Symbol Definition
t0 Theageofconcreteatthetimeofloading
t0,T Temperatureadjustedageofconcreteatloadingindays
tef,i Effectivewallthickness(torsion)
tinf Thicknessofthebottomflangeofthesection
ULS Ultimatelimitstate(s)–associatedwithcollapseorotherformsofstructuralfailure
u Perimeterofconcretecross-section,havingareaAc
u Perimeterofthatpartwhichisexposedtodrying
u Circumferenceofouteredgeofeffectivecross-section(torsion)
u Componentofthedisplacementofapoint
u0 Perimeteradjacenttocolumns(punchingshear)
u1 Basiccontrolperimeter,(at2dfromfaceofload)(punchingshear)
u1* Reducedcontrolperimeteratperimetercolumns(at2dfromfaceofload)(punchingshear)
ui Lengthofthecontrolperimeterunderconsideration(punchingshear)
uk PerimeteroftheareaAk(torsion)
uout Perimeteratwhichshearreinforcementisnolongerrequired
V Shearforce
VEd Designvalueoftheappliedshearforce
VEd,red Appliedshearforcereducedbytheforceduetosoilpressurelessselfweightofbase(punchingshear,foundations)
VRd,c Shearresistanceofamemberwithoutshearreinforcement
VRd,max Shearresistanceofamemberlimitedbythecrushingofcompressionstruts
VRd,s Shearresistanceofamembergovernedbytheyieldingofshearreinforcement
v Transverseshearorcomponentofthedisplacementofapoint
vEd Punchingshearstress
vEd Shearstressforsectionswithout shearreinforcement(=VEd/bwd)
vEd,z Shearstressforsectionswith shearreinforcement(=VEd/bwz=VEd/bw0.9d)
vRd,c Designshearresistanceofconcretewithoutshearreinforcementexpressedasastress
vRd,cs Designpunchingshearresistanceofconcretewith shearreinforcementexpressedasastress(punchingshear)
vRd,max Resistanceofconcretestrutsexpressedasastress
W1 Factorcorrespondingtoadistributionofshear(punchingshear)
w Componentofthedisplacementofapoint
wk Crackwidth
wmax Limitingcalculatedcrackwidth
X Advisorylimitofpercentageofcoupledtendonsatasection
X0,XA,XC, ConcreteexposureclassesXD,XF,XS
x Neutralaxisdepth
x Distanceofthesectionbeingconsideredfromthecentrelineofthesupport
x, y, z Co-ordinates;Planesunderconsideration
xc Depthofthecompressionzone
xu Depthoftheneutralaxisattheultimatelimitstateafterredistribution
z Leverarmofinternalforces
zcp Distancebetweencentreofgravityofconcretesectionandtendons
zs Leverarmforprestress
a Angle;Angleofshearlinkstothelongitudinalaxis;Ratio
a Longtermeffectscoefficient
x
Symbol Definition
a Ratiobetweenprincipalstresses
a Deformationparameter
a1,a2,a3 Factorsdealingwithanchorageandlapsofbarsa4,a5,a6
a1,a2,a3 Factorsusedincreepcalculations
acc(act) Acoefficienttakingintoaccountlongtermeffectsofcompressive(tensile)loadandthewayloadisapplied
acw Coefficienttakingaccountofthestateofstressinthecompressionchord
ae Effectivemodularratio
ah Reductionfactorfory
b Angle;Ratio;Coefficient
b Factordealingwitheccentricity(punchingshear)
b(fcm) Factortoallowfortheeffectofconcretestrengthonthenotionalcreepcoefficient
bH Coefficentdependingontherelativehumidityandthenotionalmembersize
b(t0) Factortoallowfortheeffectofconcreteageatloadingonthenotionalcreepcoefficient
b(t,t0) Coefficienttodescribethedevelopmentofcreepwithtimeafterloading
g Partialfactor
gA Partialfactorforaccidentalactions,A
gC Partialfactorforconcrete
gC,fat Partialfactorforfatigueofconcrete
gF Partialfactorforactions,F
gF,fat Partialfactorforfatigueactions
gf Partialfactorforactionswithouttakingaccountofmodeluncertainties
gg Partialfactorforpermanentactionswithouttakingaccountofmodeluncertainties
gG Partialfactorforpermanentactions,G
gM Partialfactorforamaterialproperty,takingaccountofuncertaintiesinthematerialpropertyitself,ingeometricdeviationandinthedesignmodelused
gP Partialfactorforactionsassociatedwithprestressing,P
gQ Partialfactorforvariableactions,Q
gS Partialfactorforreinforcingsteelorprestressingsteel
gS,fat Partialfactorforreinforcingorprestressingsteelunderfatigueloading
gSH Partialfactorforshrinkage
d Ratiooftheredistributedmomenttotheelasticbendingmoment.
ec Compressivestraininconcrete
ec1 Compressivestrainintheconcreteatthepeakstressfc
ec2 Compressivestrainlimitinconcreteforconcreteinpureaxialcompressionorstraininconcreteatreachingmaximumstrengthassuminguseoftheparabolic-rectangularrelationship
ec3 Compressivestrainlimitinconcreteforconcreteinpureaxialcompressionorstraininconcreteatreachingmaximumstrengthassuminguseofthebilinearstress-strainrelationship
eca Autogenousshrinkagestrain
ecc Creepstrain
ecd Dryingshrinkagestrain
ecm Meanstraininconcretebetweencracks
ecs Totalshrinkagestrain
ecu Ultimatecompressivestrainintheconcrete
ecu2 Ultimatecompressivestrainlimitinconcretewhichisnotfullyinpureaxialcompressionassuminguseoftheparabolic-rectangularstress-strainrelationship(numericallyecu2=ecu3)
xi
Symbol Definition
ecu3 Ultimatecompressivestrainlimitinconcretewhichisnotfullyinpureaxialcompressionassuminguseofthebilinearstress-strainrelationship
ep(0) Initialstraininprestressingsteel
Dep Changeinstraininprestressingsteel
es Straininreinforcingsteel
esm Meanstraininreinforcement
eu Strainofreinforcementorprestressingsteelatmaximumload
eud Designlimitforstrainforreinforcingsteelintension= 0.9euk
euk Characteristicstrainofreinforcement(orprestressingsteel)atmaximumload
ey Reinforcementyieldstrain
n Factordefiningeffectivestrength(=1for≤C50/60)
n1 Coefficientforbondconditions
n2 Coefficientforbardiameter
np1 Coefficientthattakesintoaccountthetypeoftendonandthebondsituationatrelease
y Angle;Angleofcompressionstruts(shear)
yfat Inclinationofcompressivestruts
yi Inclinationusedtorepresentimperfections
l Slendernessratio
l Damageequivalentfactorsinfatigue
l Factordefiningtheheightofthecompressionzone(=0.8for≤C50/60)
llim Limitingslendernessratio(ofcolumns)
m Coefficientoffrictionbetweenthetendonsandtheirducts
m Characteristicvalueofthetensilestrengthofprestressingsteel
v Poisson'sratio
v1 Strengthreductionfactorforconcretecrackedinshear
j Creepredistributionfunction
j Bondstrengthratio
j1 Adjustedareaofbondstrength
r Requiredtensionreinforcementratio.AssumeAs/bd
r Ovendrydensityofconcreteinkg/m3
r' Reinforcementratioforrequiredcompressionreinforcement,As2/bd
r0 Referencereinforcementratiofck0.5x10–3
r1 Percentageofreinforcementlappedwithin0.65l0fromthecentrelineofthelapbeingconsidered
r1000 Valueofrelaxationloss(in%)at1000hoursaftertensioningandatameantemperatureof20°C
rl Reinforcementratioforlongitudinalreinforcement
rw Reinforcementratioforshearreinforcement
sc Compressivestressintheconcrete
scp Compressivestressintheconcretefromaxialloadorprestressing
scu Compressivestressintheconcreteattheultimatecompressivestrainecu
sgd Designvalueofthegroundpressure
spi Theabsolutevalueofinitialprestress
spm0 Theabsolutevalueofinitialprestressduringpost-tensioning
sRd,max Designstrengthofconcretestrut
ss StressinreinforcementatSLS
ss Absolutevalueofthemaximumstresspermittedinthereinforcementimmediatelyaftertheformationofthecrack
xii
Symbol Definition
ssc(sst) Stressincompression(andtension)reinforcement
ssd Designstressinthebarattheultimatelimitstate
ssr Stressinthetensionreinforcementcalculatedonthebasisofacrackedsectionundertheloadingconditionscausingfirstcracking
t Torsionalshearstress
F DynamicfactoraccordingtoBSEN1991-2
h0 Notionalcreepcoefficient
h(∞,t0) Finalvalueofcreepcoefficient
hef Effectivecreepfactor
hfat Damageequivalentimpactfactorinfatigue
hnl(∞,t0) Non-linearnotionalcreepcoefficient
hp Equivalentdiameteroftendon
h(t,t0) Creepcoefficient,definingcreepbetweentimestandt0,relatedtoelasticdeformationat28days
hRH Factortoallowfortheeffectofrelativehumidityonthenotionalcreepcoefficient
f Bardiameter;Diameterofprestressingduct
feq Equivalentbardiameter
fm Mandreldiameter
fn Equivalentdiameterofabundleofreinforcingbars
X Ageingcoefficient
c Factorsdefiningrepresentativevaluesofvariableactions
c0 Combinationvalueofavariableaction(e.g.usedwhenconsideringULS)
c1 Frequentvalueofavariableaction(e.g.usedwhenconsideringwhethersectionwillhavecrackedornot)
c2 Quasi-permanentvalueofavariableaction(e.g.usedwhenconsideringdeformation)
w Mechanicalreinforcementratio=As fyd/Ac fcd≤1
1
Introduction
1 IntroductionBS EN 1992-1-1 (Eurocode 2: Design of concrete structures Part 1-1[1]) sets out general rulesfor the design of concrete structures and rules for the design of buildings. BS EN 1992-2(Eurocode 2 - Part 2 Concrete bridges - Design and detailing rules)[2] provides additional oramendedguidancetoPart1-1forbridgestructures.
TheaimofthisConcise Eurocode 2 for BridgesistodistilfromallrelevantpartsofBSEN1992andtheUKNationalAnnexes materialthatwillbecommonlyusedinthedesignofnormalbridgestructures. Each country can publish non-contradictory, complementary information, and forconcretebridgedesign,PD6687,Part2 [3]givesusefulguidance.Materialfromthisdocumentisalsoincludedwhereappropriate,andpresentedonapaleyellowbackgroundtodistinguishitfromthemaintext.
As far as possible, the Eurocode clauses are repeated verbatim. One of the objectives is toembed the UK National Annex values into the document for ease of use. Due to the wayNationally Determined Parameters (NDPs) are introduced in the Eurocodes it has beennecessaryinsomeplacestomodifythetextforclarityofreading.IthasnotbeentheintentiontomodifythemeaningofthetextandclearlyifthereisanydoubtastothemeaningthentheoriginalEurocodeversionshouldbeadopted.
Further,someoftheoriginaltexthasbeenmodifiedtoreduceitslength,whilekeepingthesamemeaning.Inthiscasethetexthasbeengivenagreybackgroundtodrawthereader’sattentionto the fact that the text is not strictly from theCode. Likewise other text, derived formulae,tablesandillustrationsthatareprovidedtoassistthedesignersbutthatarenottakendirectlyfrom the original have been given a grey background.As before, it is intended to convey theoriginalmeaningandwhereanydoubtexiststhemeaningofEurocode2shouldbeadopted.
The NDPs are recognition that each Member State of the EU is responsible for determiningmatters such as safety and current practice and allow individual countries to set their ownvalues.Asnotedabove,theUKvalueshavebeenadoptedthroughout,buthavebeenhighlightedwithagreenbackgroundsothatitiscleartothereaderwhatNDPvaluehasbeenused.
Guide to presentation
Greyshadedtext,tablesandfigures
ModifiedEurocode2textandadditionaltext,derivedformulae,tablesandillustrationsnot fromEurocode2
Yellowshadedtext,tablesandfigures
AdditionaltextfromPD6687[6]orPD6687-2[3]
BS EN 1992-1-1 6.4.4
Relevantcodeandclausesorfigurenumbers
BS EN 1992-1-1 NA FromtherelevantUKNationalAnnex
BS EN 1992-1-1 6.4.4 & NA FrombothEurocode2-1-1andUKNationalAnnex
Section 5.2 Relevantpartsofthispublication
1.0 NationallyDeterminedParameter.UKvalueshavebeenusedthroughout
For ease of reference, this guide is repeated on the inside back cover.
2
Scope
Thispublicationisintendedtocoverthedesignofatypicalbridge;thereareparticulartypesofbridgessuchassuspensionbridgesandsegmentalbridgesthatshouldnotbedesignedwithoutreference to theCode itself. It should also be noted that not every method presented in theCodeisgivenhere.Generally,thesimplestandmoreconservativemethodshavebeenincludedandthereforethereadermayfindtherearebenefitstobegainedbyusingothermethodsandshouldconsulttheCodeontheseoccasions.
Thispublicationdoesnotcoverthemethodofdesigningconcreteelementsusingmembranerules.Membraneelementsmaybeusedforthedesignoftwo-dimensionalconcreteelementssubject to a combination of internal forces evaluated by means of a linear finite elementanalysis.ThereadershouldrefertoBSEN1992-2AnnexLL inconjunctionwithAnnexFandCl. 6.109 for detailed guidance. For the design or verification of shell elements subject tobending alone (i.e. with zero membrane forces) the approaches given byWoodArmer[4] andDenton&Burgoyne[5]maygenerallybeused.
1.1
3
Basisofdesign
Basis of design
General
BSEN1992-1-1[1]andBSEN1992-2[2]shouldbeusedinconjunctionwithBSEN1990:Basis of structural design[7],which:
■ Establishesprinciplesandrequirementsforthesafety,serviceabilityanddurabilityofstructures.
■ Describesthebasisfortheirdesignandverification.■ Givesguidelinesforrelatedaspectsofstructuralreliability.
Basic requirements
General
Astructureshouldbedesignedandexecuted(constructed)insuchawaythatitwill,duringitsintendedlife,withappropriatedegreesofreliabilityandinaneconomicalway:
■ Sustainallactionsandinfluenceslikelytooccurduringexecutionanduse.■ Meetthespecifiedserviceabilityrequirementsforastructureorastructuralmember.
Itshouldbedesignedtohaveadequatestructuralresistance,serviceabilityanddurability.
Astructureshouldbedesignedandexecutedinsuchawaythatitwillnotbedamagedbyeventssuchasexplosion,impactandtheconsequencesofhumanerrors,toanextentdisproportionatetotheoriginalcause.
Avoidance of damage
Potential damage should be avoided or limited by appropriate choice of one or more of thefollowing:
■ Avoiding,eliminatingorreducingthehazardstowhichthestructurecanbesubjected.■ Selectingastructuralformwhichhaslowsensitivitytothehazardsconsidered.■ Selectingastructuralformanddesignthatcansurviveadequatelytheaccidentalremoval
ofanindividualstructuralmemberoralimitedpartofthestructureortheoccurrenceoflocaliseddamage.
■ Avoidingasfaraspossiblestructuralsystemsthatcancollapsewithoutwarning.■ Tyingthestructuralmemberstogether.
Limit states principles
BSEN1990impliesthatthedesignshouldbeverifiedusinglimitstatesprinciples.
Anindicativevalueof120yearsisgivenintheUKNationalAnnexforthedesignworkinglifeofbridges.ItcangenerallybeassumedthattheguidancegiveninBS8500[8]foratleasta100-year'intendedworkinglife'willbeappropriateforan'indicativedesignworkinglife'of120years.
BS EN 1990 2.1(1), (2) & (4)
BS EN 1990 1.1.1(1)
BS EN 1992-1-1 1.1.1(3)
BS EN 19902.1(5)
BS EN 19903.1(1)
BS EN 19902.3 & NA
2
2.1
2.2
2.2.1
2.2.2
2.2.3
4
Limit state design
Limit states are states beyond which the structure no longer fulfils the relevantdesigncriteria:
■ Ultimatelimitstates(ULS)areassociatedwithcollapseorotherformsofstructuralfailure.
■ Serviceabilitylimitstates(SLS)correspondtoconditionsbeyondwhichspecifiedservicerequirementsarenolongermet.
Limitstatesshouldbeverifiedinallrelevantdesignsituationsselected,takingintoaccountthecircumstancesunderwhichthestructureisrequiredtofulfilitsfunction.
Design situations
Normally,innon-seismiczones,thefollowingdesignsituationsshouldbeconsidered:
■ Persistentsituationswhichrefertotheconditionsofnormaluse.■ Transientsituationswhichrefertotemporaryconditions,suchasduringexecutionorrepair.■ Accidentalsituationswhichrefertoexceptionalconditionsapplicabletothestructureorto
itsexposuree.g.fire,explosion,impactortheconsequencesoflocalisedfailure.
Actions
Actionsrefertoasetofforces(loads)appliedtothestructure(directaction),ortoasetofimposeddeformationsoraccelerationscaused,forexample,bytemperaturechanges,moisturevariation,unevensettlementorearthquakes(indirectaction).
■ Permanentactionsrefertoactionsforwhichthevariationinmagnitudewithtimeisnegligible.
■ Variableactionsareactionsforwhichthevariationinmagnitudewithtimeisnotnegligible.
■ Accidentalactionsareactionsofshortdurationbutofsignificantmagnitudethatareunlikelytooccuronagivenstructureduringthedesignworkinglife.
Thecharacteristicvalue,Fk,ofanactionisitsmainrepresentativevalueandshallbespecifiedby:
■ Ameanvalue –generallyusedforpermanentactions.■ Anuppervalue withanintendedprobabilityofnotbeingexceeded orlowervalue
withanintendedprobabilityofbeingachieved–normallyusedforvariableactionswith knownstatisticaldistributions,suchaswindorsnow.
■ Anominalvalue –usedforsomevariableandaccidentalactions.
The values of actions given in the various parts of BS EN 1991: Actions on structures[9] aretakenascharacteristicvalues.
Verification
Verification,usingthepartialfactormethod,isdetailedinBSEN1990[4].Inthismethoditisverifiedthat,inallrelevantdesignsituations,norelevantlimitstateisexceededwhendesignvaluesforactionsandresistancesareusedinthedesignmodels.
BS EN 19903.1 & 3.4
BS EN 19903.2
BS EN 19901.5.3.1
BS EN 19901.5.3.3
BS EN 19901.5.3.4
BS EN 19901.5.3.5
BS EN 19904.1.2(1)
BS EN 1990
BS EN 1991
2.3
2.3.1
2.3.2
2.3.3
5
BasisofdesignBasisofdesign
Design values of actions
Thedesignvalue,Fd,ofanaction,F,canbeexpressedingeneraltermsasFd=gFcFk
wheregF =partialfactorfortheactionwhichtakesaccountofthepossibilityofunfavourable deviationsoftheactionvaluesfromtherepresentativevalues.c =afactorfortheaction c canhavethevalue1.0,c0orc1orc2 whichisusedtoobtainthecharacteristic,
combination,frequentandquasi-permanentvaluesrespectively.Itadjuststhevalueoftheactiontoaccountforthejointprobabilityoftheactionsoccurringsimultaneously.
SeeTables2.1to2.3whicharederivedfromBSEN1990anditsNationalAnnex[7a].Fk= characteristicvalueofanaction.
Table 2.1
Values of c factors for road bridges
Action Symbol c0 c1 c2
Traffic loads (see BS EN 1991-2, table 4.4)
gr1aa TS 0.75 0.75 0
UDL 0.75 0.75 0
Pedestrianandcycle-trackloadsb 0.40 0.40 0
gr1ba Singleaxle 0 0.75 0
gr2 Horizontalforces 0 0 0
gr3 Pedestrianloads 0 0.40 0
gr4 Crowdloading 0 0.75 0
gr5c VerticalforcesfromSVandSOVVehicles 0 1.0 0
Wind forces F Wk Persistentdesignsituations 0.50 0.20 0
F Wk Duringexecution 0.80 – 0
F* W Duringexecution 1.0 – 0
Thermal actions T k 0.60d 0.60 0.50
Snow loads Q Sn,k (duringexecution) 0.80 – –
Construction loads Qc 1.0 – 1.0
Key
a Thevaluesofc0,c1andc2forgr1aandgr1baregivenforroadtrafficcorrespondingtoadjustingfactorsaQi,aqi ,aqrandbQ=1
b Thevalueofthepedestrianandcycle-trackload,giveninTable4.4aofEN1991-2,isa'reduced'valueaccompanyingthecharacteristicvalueofLM1andshouldnotbefactoredagainbyc1.However,whengr1aiscombinedwithleadingnon-trafficactions,thisvalueshouldbefactoredbyc0
c InaccordancewithBSEN1991-2Cl.4.5.2,thefrequentvalueofgr5doesnotneedtobeconsidered.
d Thec0valueforthermalactionsmayinmostcasesbereducedto0forultimatelimitstatesEQU,STRandGEO
Table 2.2
Values of c factors for footbridges
Action Symbol c0 c1 c2
Traffic loads gr1 0.4 0.4 0
Qfwk0 0 0
gr2 0 0 0
Wind forces F Wk0.3 0.2 0
Thermal actions T k 0.6a 0.6 0.5
Snow loads Q Sn,k(duringexecution) 0.8 – 0
Construction loads Qc 1.0 – 1.0
Key
a Thec0valueforthermalactionsmayinmostcasesbereducedto0forultimatelimitstatesEQU,STRandGEO
BS EN 1990 NA table NA. A.2.1
BS EN 1990 NA table NA. A.2.2
2.3.4
BS EN 19906.3.1
6
Table 2.3
Values of c factors for railway bridges
Actions c0 c1 c2a
Individual components of traffic actionsb
LM71 0.80 c 0
SW/0 0.80 c 0
SW/2 0 1.00 0
Unloadedtrain 1.00 – –
HSLM 1.00 1.00 0
TrackingandbrakingCentrifugalforcesInteractionforcesduetodeformationunderverticaltrafficloads
Individualcomponentsoftrafficactionsindesignsituationswherethetrafficloadsareconsideredasasingle(multi-directional)leadingactionandnotasgroupsofloadsshouldusethe
samevaluesofcfactorsasthoseadoptedfortheassociatedverticalloads
Nosingforces 1.00 0.80 0
Non-publicfootpathsloads 0.80 0.50 0
Realtrains 1.00 1.00 0
Horizontalearthpressureduetotrafficloadsurcharge 0.80 c 0
Aerodynamiceffects 0.80 0.50 0
Main traffic actions (groups of loads)
gr11(LM71+SW/0) Max.vertical1withmax.longitudinal 0.80 0.80 0
gr12(LM71+SW/0) Max.vertical2withmax.transverse
gr13(Braking/traction) Max.longitudinal
gr14(Centrifugal/nosing) Max.lateral
gr15(Unloadedtrain) Lateralstabilitywith'unloadedtrain'
gr16(SW/2) SW/2withmax.longitudinal
gr17(SW/2) SW/2withmax.transverse
gr21(LM71+SW/0) Max.vertical1withmax.longitudinal 0.80 0.70 0
gr22(LM71+SW/0) Max.vertical2withmax.transverse
gr23(Braking/traction) Max.longitudinal
gr24(Centrifugal/nosing) Max.lateral
gr26(SW/2) SW/2withmax.longitudinal
gr27(SW/2) SW/2withmax.transverse
gr31(LM71+SW/0) Additionalloadcases 0.80 0.60 0
Other operating actions
Aerodynamiceffects 0.80 0.50 0
Generalmaintenanceloadingfornon-publicfootpaths 0.80 0.50 0
Wind forces d F Wk0.75 0.50 0
F** W 1.00 0 0
Thermal actionse T K 0.60 0.60 0.50
Snow loads Q Sn,k (duringexecution) 0.80 – 0
Construction loads Qc 1.00 – 1.00
Key
a Ifdeformationisbeingconsideredforpersistentandtransientdesignsituations,c2shouldbetakenequalto1.00forrailtrafficactions.Forseismicdesignsituations,seeTableNAA2.5ofBSEN1990NA
b Minimumcoexistantfavourableverticalloadwithindividualcomponentsofrailtrafficactions(e.g.centrifugal,tractionorbraking)is0.5LM71,etc.
c 0.8 if1trackonlyisloaded
0.7 if2tracksaresimultaneouslyloaded
0.6 if3ormoretracksaresimultaneouslyloadedd Whenwindforcesactsimultaneouslywithtrafficactions,thewindforcec0FWk shouldbetakenasnogreaterthanF** W
(seeBSEN1991-1-4).SeeA2.2.4(4)ofBSEN1990e SeeBSEN1991-1-5
BS EN 1990 table A.2.3
7
BasisofdesignBasisofdesign
Combinations of actions
Ultimate limit states
Thefollowingultimatelimitstatesshallbeverifiedasrelevant:
EQU Lossofstaticequilibriumofthestructureoranypartofitconsideredasarigidbody.STR Internalfailureorexcessivedeformationofthestructureorstructuralmembers.GEO Failureorexcessivedeformationofthestructurewherethestrengthsofsoilorrockare
significantinprovidingresistance.FAT Fatiguefailureofthestructureorstructuralmembers.
ThepartialfactorsandcombinationsofactionsfortheselimitstatesaregiveninTables2.4to2.7.
Table 2.4Recommended partial factors
Action EQU (Set A) STR/GEO (Set B) STR/GEO (Set C)
Permanent actions gG,sup gG,inf gG,sup gG,inf gG,sup gG,inf
Concrete self-weight 1.05 0.95 1.35 0.95 1.00 1.00
Steel self-weight 1.05 0.95 1.20 0.95 1.00 1.00
Superimposed dead a 1.05 0.95 1.20 0.95 1.00 1.00
Road surfacing a 1.05 0.95 1.20 0.95 1.00 1.00
Weight of soil 1.05 0.95 1.35 0.95 1.00 1.00
Self-weight of other materials listed in BS EN 1991-1-1, tables A.1-A.6
1.05 0.95 1.35 0.95 1.00 1.00
Creep and shrinkage – – 1.20 0 1.00 0
Settlement (linear structural analysis)
– – 1.20 0 1.00 0
Settlement (non-linear structural analysis)
– – 1.35 0 1.00 0
Variable actions (gQ) Unfavourable Favourable Unfavourable Favourable Unfavourable Favourable
Road traffic actions (gr1a, gr1b, gr2, gr5, gr6)
1.35 0 1.35 0 1.15 0
Pedestrian actions (gr3, gr4)
1.35 0 1.35 0 1.15 0
Rail traffic actions (LM71, SW/0, HSLM)
1.45 0 1.45 0 1.25 0
Rail traffic actions (SW/2 and other load models representing controlled exceptional traffic)
1.40 0 1.40 0 1.20 0
Rail traffic actions (real trains)
1.70 0 1.70 0 1.45 0
Wind actions 1.70 0 1.70 0 1.45 0
Thermal actions 1.55 0 1.55 0 1.30 0
Key
a SeeTableNA.1ofBSEN1991-1-1[9]forguidanceonthicknessesforballast,waterproofing,surfacesandothercoatings.NoteFordesignvaluesforself-weightofwater,groundwaterpressureandearthpressuresrefertoBSEN1997-1.
BS EN 19906.4.1
2.3.5
BS EN 1990 tables NA.A.2.4(A), (B) & (C)
8
Table 2.7Combinations of fatigue actions
Action Permanent actions Prestress Leading variable action
Accompanying variable actions
Fatigue actionFavourable Unfavourable
Non-cyclic Gk,j,inf Gk,j,supP c1,1Qk,1 c2,iQk,i
–
Cyclic Gk,j,inf Gk,j,supP c1,1Qk,1 c2,iQk,i Qfat
Serviceability limit states
ThecombinationsofactionsfortheserviceabilitylimitstatearegiveninTable2.8.
Table 2.8Combinations of actions for the serviceability limit state
Combination Permanent actions Prestress Variable actions
Favourable Unfavourable Leading Others
Characteristic Gk,j,sup Gk,j,infP Qk,1 c0,iQk,i
Frequent Gk,j,sup Gk,j,infP c1,1Qk,1 c2,iQk,i
Quasi-permanent Gk,j,sup Gk,j,infP c2,1Qk,1 c2,iQk,i
Actions to consider
Thermaleffects,differentialsettlements/movements,creepandshrinkageshouldbetakenintoaccountwhencheckingserviceabilitylimitstates.
Thermaleffects,differentialsettlements/movements,creepandshrinkageshouldbeconsideredforultimatelimitstatesonlywheretheyaresignificant(e.g.fatigueconditions,intheverificationofstabilitywheresecondordereffectsareofimportance,etc.).Inothercasestheyneednotbeconsidered,providedthattheductilityandrotationcapacityoftheelementsaresufficient.
Wherethermaleffectsaretakenintoaccounttheyshouldbeconsideredasvariableactionsandappliedwithapartialfactorandcfactor,whichcanbedeterminedfromBSEN1990AnnexA2.
2.3.6
Table 2.5Combinations of actions for EQU, STR and GEO limit states
Persistent and transient design situation
Permanent actions Prestress Leading variable action
Accompanying variable actionsUnfavourable Favourable
Exp. (6.10) gG,supGkj,sup g G,infGkj,infg PP gQ,1Qk,1 g Q,ic 0,iQk,i
NoteForpartialfactorsseeTable2.4(exceptseeTable2.9forg P)
Table 2.6Combinations for accidental situations
Accidental design situation
Permanent actions Prestress Accidental action
Accompanying variable actions
Unfavourable Favourable Main Others
Exp. (6.11a/b) Gk,j,sup Gk,j,infP Ad
c1,1 Qk,1 c2,iQk,i
BS EN 1992-1-12.3.1.2(3)
BS EN 1990table A2.5
BS EN 1992-1-16.8.3
BS EN 1990table A2.6
BS EN 1992-1-12.3.1.2, 2.3.1.3& 2.3.2.2
BS EN 1990 tables NA.A.2.4(A), (B) & (C)
9
Basisofdesign
Differentialsettlements/movementsofthestructureduetosoilsubsidenceshouldbeclassifiedasapermanentaction,Gsetwhichis introducedassuchincombinationsofactions.Apartialsafetyfactorforsettlementeffectsshouldbeapplied.
When creep is taken into account its design effects should be evaluated under the quasi-permanentcombinationofactionsirrespectiveofthedesignsituationconsideredi.e.persistent,transientoraccidental.Inmostcasestheeffectsofcreepmaybeevaluatedunderpermanentloadsandthemeanvalueofprestress.
Thedesignvaluesforvehicle impactsonsupportingstructuresandsubstructuresaregiveninBSEN1991-1-1[9]section4.3.ThedeisgnvaluesforvehicleimpactsonparapetsaregiveninBSEN1991-2[9]section4.8.
AppropriatevaluesforpartialactionsaregiveninTable2.9
Table 2.9Values for partial factors applied to actions
Action Ultimate limit state Servicability limit state
STR/GEO EQU FAT Favourable Unfavourable
Favourable Unfavourable Favourable Unfavourable
Shrinkage gSH=0 gSH=1.0 – – – – –
Prestress effects gP,fav=0.9 gP,unfav=1.1 gP,fav=0.9 gP,unfav=1.2 – rinf=1.0 rsup=1.0
Fatigue – – – – gF,fat=1.0 – –
Material properties
Material properties are specified in terms of their characteristic values, which in generalcorrespond to a defined fractile of an assumed statistical distribution of the propertyconsidered(usuallythelower5%fractile).
ThevaluesofgCandgS,partialfactorsformaterials,areindicatedinTable2.10.
Table 2.10Partial factors for materials
Design situation gC – concrete gS – reinforcing steel gS – prestressing steel
ULS – Persistent and transient 1.50 1.15 1.15
Accidental 1.20 1.00 1.00
Fatigue 1.50 1.15 1.15
SLS 1.00 1.00 1.00
Assumptions
InadditiontotheassumptionsinBSEN1990,itisassumedthat:
■Structuresaredesignedbyappropriatelyqualifiedandexperiencedpersonnel.■Adequatesupervisionandqualitycontrolisprovided.■Constructioniscarriedoutbypersonnelhavingtheappropriateskillandexperience.■MaterialsandproductswillbeusedasspecifiedinEurocode2orintherelevantmaterialor
productspecifications.■Thestructurewillbeadequatelymaintainedandwillbeusedinaccordancewiththe
designbrief.■TherequirementsforexecutionandworkmanshipgiveninENV13670[10]arecompliedwith.
2.3.7
2.4
BS EN 1992-1-12.3.1.3(1) & (4)
BS EN 1992-1-12.3.2.2(3)
BS EN 1992-1-1 2.4.2.4(1) & NA
BS EN 1992-1-1 table 2.1 N & NA
BS EN 1992-1-11.3
10
2.5
AtthetimeofwritingBSEN13670[11] isexpectedtobepublishedinlate2009,andwillreplace ENV 13670. Once published it is anticipated that standard specifications will beupdatedtorefertoit.Intheinterimexistingspecificationsshouldbeadapted.
Foundation design
ThedesignofconcretefoundationsissubjecttoEurocode7[12]forthegeotechnicalaspectsandtoEurocode2forthestructuralconcretedesign.FurtherguidanceonthegeotechnicaldesigncanbefoundinPD6694-1[13].
Eurocode7iswiderangingandprovidesalltherequirementsforgeotechnicaldesign.Itstatesthatnolimitstatee.g.equilibrium,stability,strengthorserviceability,asdefinedbyBSEN1990,shallbeexceeded.TherequirementsforULSandSLSdesignmaybeaccomplishedbyusing,inanappropriatemanner,thefollowingaloneorincombination:
■ Calculations.■ Prescriptivemeasures.■ Testing.■ Observationalmethods.
The foundation design and the derivation of design resistance are covered by theGeotechnical Design Report. For simple structures, this report can be combined with theground investigation report but it is still a distinct requirement. Both the ULS and SLSconditions must be met but the definition of the SLS criteria is not possible without theliaisonwiththebridgedesignerandafullEurocode7compatibledesigncannotbecarriedoutbyapartyinisolationfromtherestofthestructuredesignteam.
BS EN 19972.1(4)
BS EN 19972.4.6.4
11
Materials
BS EN 1992-1-1 3.1.2(1)
BS EN 1992-1-1 4.4.1.2(5) & NA
BS EN 1992-1-1 table 3.1
BS EN 1992-23.1.2 (102) & NA
BS EN 1992-1-13.1.2 (2) & NA
BS EN 1992-1-1 3.1.6(1) & NA
BS EN 1992-1-1 3.1.3(4)
BS EN 1992-1-1 3.1.3(5)
3
3.1
3.1.1
Materials
Concrete
Strength and other properties
The compressive strength is denoted by concrete strength classes which relate to thecharacteristic(5%)cylinderstrengthfck,orthecubestrengthfck,cube,inaccordancewithBSEN206-1Concrete: Specification, performance, production and conformity [14].
IntheUK,BS8500 [8]complementsBSEN206-1andtheguidancegivenintheformershouldbefollowed.
Concrete strength classes and properties are shown inTable 3.1. In the notation used forcompressivestrengthclass,‘C’referstonormalweightconcrete,thefirstnumberreferstothecylinderstrengthfckandthesecondtocubestrengthfck,cube.
Thestrengthclasses(C)inBSEN1992-2aredenotedbythecharacteristiccylinderstrengthfckdetermined at 28 days with a minimum value ofC25/30 and a maximum value ofC70/85.The shear strength of concrete classes higher thanC50/60 should be determined by tests orlimitedtothatofC50/60.
Thevalueofthedesigncompressivestrengthofconcrete,fcd,isdefinedas:
fcd=accfck/gC
where fck =characteristiccompressivecylinderstrengthofconcreteat28days gC =partialfactorforconcrete(SeeTable2.9) acc =acoefficienttakingaccountoflongtermeffectsonthecompressivestrengthandof
unfavourableeffectsresultingfromthewaytheloadisapplied. IntheUKacciseither1.0or0.85dependingonthesituation.Thecorrectvaluesareusedintheappropriateclausesbelow.Generallyitis1.0forshearand0.85inothercircumstances
Thevalueofconcretedesigntensilestrengthfctdisdefinedas:fctd= 1.0 fctk,0.05/gC
where fctk,0.05=5%fractilevalueofaxialtensilestrengthofconcrete
Poisson'sratiomaybetakenequalto0.2foruncrackedconcreteand0forcrackedconcrete.
Unlessmoreaccurateinformationisavailable,thelinearcoefficientofthermalexpansionmaybetakenequalto10x10–6K–1.
Table 3.1Concrete strength classes and properties
Property Strength class (MPa)
C25/30 C30/37 C35/45 C40/50 C45/55 C50/60 C55/67 C60/75 C70/85 C28/35a C32/40a
fck 25 30 35 40 45 50 55 60 70 28 32
fck, cube 30 37 45 50 55 60 67 75 85 35 40
fcm 33 38 43 48 53 58 63 68 78 36 40
fctm 2.6 2.9 3.2 3.5 3.8 4.1 4.2 4.4 4.6 2.8 3.0
fctk,0.05 1.8 2.0 2.2 2.5 2.7 2.9 3.0 3.1 3.2 1.9 2.1
fctk,0.95 3.3 3.8 4.2 4.6 4.9 5.3 5.5 5.7 6.0 3.6 3.9
Ecm,(GPa) 31 33 34 35 36 37 38 39 41 32 33
KeyaDeriveddata
BS EN 1992-1-1 table 3.1
12
BS EN 1992-1-13.1.4(2)
BS EN 1992-1-1B.1(1)
BS EN 1992-1-1B.1(2)
Creep
Thecreepcoefficient,h(t,t0)isrelatedtoEc,thetangentmodulus,whichmaybetakenas
1.05Ecm.
Thecreepcoefficienth(t,t0)maybeobtainedfromFigure3.1ofBSEN1992-1-1,orcalculatedfrom:
h(t,t0)=h0bc(t,t0)
where h0= notionalcreepcoefficientandmaybeestimatedfrom:
= hRHb(fcm)b (t0)
where hRH = factortoallowfortheeffectofrelativehumidityonthenotionalcreep
coefficient: = 1+1–RH/100forfcm≤35MPa 0.1h0
1/3
= [1+a1(1–RH/100)]a2forfcm>35MPa 0.1h0
1/3
RH =relativehumidityoftheambientenvironmentin% b (fcm) =factortoallowfortheeffectofconcretestrengthonthenotionalcreep
coefficient =16.8/fcm
0.5
fcm =meancompressivestrengthofconcreteinMPaattheageof28days
b (t0) =factortoallowfortheeffectofconcreteageatloadingonthenotionalcreepcoefficient
=1/(0.1+t00.20) h0 =notionalsizeofthememberinmm =2Ac/u Ac =cross-sectionalarea u =perimeterofthememberincontactwiththeatmosphere bc(t,t0)=coefficienttodescribethedevelopmentofcreepwithtimeafter loading =[(t – t0)/(bH+t – t0)]0.3
where t =ageofconcreteindaysatthemomentconsidered t0 =ageofconcreteatloadingindays t – t0 =non-adjusteddurationofloadingindays bH =coefficient depending on the relative humidity (RH in %) and the
notionalmembersize(h0inmm) =1.5[1+(0.012RH)18]h0+250≤1500forfcm≤35MPa =1.5[1+(0.012RH)18]h0+250a3≤1500a3forfcm>35MPa a1 =(35/fcm)0.7
a2 =(35/fcm)0.2
a3 =(35/fcm)0.5
Theeffectoftypeofcementonthecreepcoefficientofconcretemaybetakenintoaccountbymodifyingtheageofloadingt0accordingtothefollowingExpression:t0=t0,T(9/(2+t0,T
1.2)+1)a≥0.5
where t0,T =temperatureadjustedageofconcreteatloadingindays(seebelow) a =powerwhichdependsontypeofcement =-1forcementClassS(cementClassCEM32.5N) =0forcementClassN(cementClasses32.5R&CEM42.5N) =1forcementClassR(cementClassesCEM42.5R,CEM52.5N&CEM52.5R)
3.1.2
13
Materials
CementclassescanbespecifiedusingBSEN197-1[15].WherethecementClassisnotknown,generally Class R may be assumed. Where the ground granulated blastfurnace slag (ggbs)contentexceeds35%ortheflyashcontentexceeds20%ofthecementcombination,ClassNmaybeassumed.Whereggbsexceeds65%orpfaexceeds35%,ClassSmaybeassumed.
The effect of elevated or reduced temperatures within the range 0–80°C on the maturity ofconcretemaybetakenintoaccountbyadjustingtheconcreteageaccordingtothefollowingExpression: ntT=Se – (4000/[273+T(Dti)]–13.65)Dt i=1
where tT =temperature-adjustedconcreteagewhichreplacestinthecorrespondingequations T(Dti ) =temperaturein°CduringthetimeperiodDti Dti =numberofdayswhereatemperatureTprevails
The mean coefficient of variation of the above predicted creep data, deduced from acomputeriseddatabankoflaboratorytestresults,isoftheorderof20%.
Thecreepdeformationofconcreteecc(∞,t0)attimet=∞foraconstantcompressivestressscappliedattheconcreteaget0,isgivenby:
ecc(∞,t0)=h(∞,t0)(sc/Ec)
Whenthecompressivestressofconcreteatanaget0exceedsthevalue0.45fck(t0)thencreepnon-linearityshouldbeconsidered.Suchahighstresscanoccurasaresultofpretensioning,e.g.in precast concrete members at tendon level. In such cases the non-linear notional creepcoefficientshouldbeobtainedasfollows:
hnl(∞,t0)=h(∞,t0)exp[1.5(ks–0.45)]
where hnl(∞,t0)=non-linearnotionalcreepcoefficient,whichreplacesh(∞,t0) ks =stress–strengthratiosc/fck(t0) sc =compressivestress fck(t0) =characteristicconcretecompressivestrengthatthetimeofloading
Shrinkage
Thetotalshrinkagestrainiscomposedoftwocomponents,thedryingshrinkagestrainandtheautogenousshrinkagestrain.Thedryingshrinkagestraindevelopsslowly,sinceitisafunctionofthe migration of the water through the hardened concrete.The autogenous shrinkage straindevelopsduringhardeningoftheconcrete:themajorpartthereforedevelopsintheearlydaysaftercasting.Autogenousshrinkage isa linearfunctionoftheconcretestrength. Itshouldbeconsideredspecificallywhennewconcreteiscastagainsthardenedconcrete.
Hencethevaluesofthetotalshrinkagestrainfollowfrom:ecs=ecd+eca
where ecs=totalshrinkagestrain ecd=dryingshrinkagestrain(seeTable3.2) eca=autogenousshrinkagestrain(seeTable3.2)
Steel reinforcement
ThepropertiesofsteelreinforcementtoBS4449:2005[16]areshowninTable3.3.ThisBritishStandardcomplementsBSEN10080[17]andAnnexCofBSEN1992-1-1.
AnnexCallowsforastrengthrangebetween400and600MPa.BS4449:2005adopts500MPa.
BS EN 1992-1-13.1.4(3)
BS EN 1992-1-13.1.4(4)
BS EN 1992-1-13.1.4(6)
BS EN 1992-1-13.2
Materials
BS EN 1992-1-1B.1(3)
3.1.3
3.2
14
Table 3.2Long-term (70-year) shrinkage strains
Concrete strength at 28 days ( fck)
Strain due to drying shrinkage (x 103)
Strain due to autogenous shrinkage (x 103)
Total shrinkage strains (x 103)
20 0.517 0.025 0.542
25 0.489 0.038 0.527
30 0.463 0.050 0.513
35 0.438 0.063 0.501
40 0.415 0.075 0.490
45 0.393 0.088 0.481
50 0.372 0.100 0.472
60 0.333 0.125 0.458
70 0.298 0.150 0.448
Notes1ThevaluesshownassumeClassRcement(ClassNandClassSwillhavelowervalues).
2Thedryingshrinkagevaluesassumeanotionalmembersize,h0,of150mm.Forh0of300mmmultiplyvaluesby0.81andforh0of500mmorgreater,multiplyvaluesby0.75.
Table 3.3Properties of reinforcement
Property Class
A B C
Characteristic yield strength fyk or f0.2k (MPa) 500 500 500
Minimum value of k = (ft /fy)k ≥1.05 ≥1.08 ≥1.15<1.35
Characteristic strain at maximum force euk (%) ≥2.5 ≥5.0 ≥7.5
NoteTablederivedfromBSEN1992-1-1AnnexC,BS4449:2005andBSEN10080.ThenomenclatureusedinBS4449:2005differsfromthatusedinAnnexCandusedhere.
ClassBorClassCreinforcementshouldbeused.Forsteelfabricreinforcement,ClassAmayalsobeusedprovideditisnottakenintoaccountintheevaluationoftheultimateresistance.
Prestressing steel
Typical prestressing strand properties are shown inTable 3.4.The manufacturer’s technicaldatasheetsshouldbereferredfordetailedinformation.
PropertiesofprestressingsteelsshouldbeinaccordancewithEN10138.However,untilthisstandardispublishedBS5896[18]maybeused.
The0.1%proofstress(fp0.1k)andthespecifiedvalueoftensilestrength(fpk)areusedtodefinethecharacteristicvaluesoftheprestressingsteels.
Thedesignvaluesfortheprestressingsteelarederivedbydividingthecharacteristicvaluesby the partial safety factor for prestressing steel gS. For ultimate limit state verification,gS=1.15forpersistentandtransientdesignsituationsand1.0foraccidentaldesignsituations.
ThemodulusofelasticityEpcanbeassumedequalto205GPaforwiresandbarsand195GPaforstrand.
BS EN 1992-1-1table C1
BS EN 1992-2 3.2.4 & NA
BS EN 1992-1-1 3.3.6(2) & (3)
BS EN 1992-1-1 3.3.2(1)
BS EN 1992-1-1 3.3.3(1)
3.3
15
MaterialsMaterials
Table 3.4Dimensions and properties of low relaxation strand and wire for prestressed concrete
Type of strand
Nominal diameter (mm)
Nominal tensile strength (MPa)
Steel area (mm²)
Nominal mass (g/m)
Characteristic breaking load (kN)
Characteristic 0.1% proof load (kN)
Characteristic load at 1% elongation (kN)
7 wire standard
15.2 1860 139 1090 259 220 228
15.2 1670 139 1090 232 197 204
12.5 1860 93 730 173 147 152
12.5 1770 93 730 164 139 144
11.0 1770 71 557 125 106 110
9.3 1860 52 408 97 82 85
9.3 1770 52 408 92 78 81
7 wire super 15.7 1860 150 1180 279 237 246
15.7 1770 150 1180 265 225 233
12.9 1860 100 785 186 158 163
11.3 1860 75 590 139 118 122
9.6 1860 55 432 102 87 90
8.0 1860 38 298 70 59 61
7 wire drawn 18.0 1770 223 1750 380 323 334
15.2 1820 165 1295 300 255 264
12.7 1860 112 890 209 178 184
Relaxation of prestressing steel
BSEN1992-1-1definesthreeclassesofrelaxation.
Class1:ordinarywireandstrandClass2:lowrelaxationwireandstrandClass3:hotrolledandprocessedbars
Thedesigncalculationofthelossesduetorelaxationoftheprestressingsteelshouldbebasedon the loss at 1000 hr (r1000) after tensioning at a mean temperature of 20°C and initialprestressof70%(0.7fpk).Thevaluesofr1000canbetakenfromthecertificateorassumedtobe:
Class1–8%Class2–2.5%Class3–4%
The relaxation loss may be obtained from manufacturer’s test certificates or they can becalculated,baseduponthefollowingequations(seealsoTable3.5):
Class1 spr tr1000spi
D5. 39 e 6.7m 10–5
1000=
0.75 (1– m)
Class2 spr tr1000spi
D0. 66 e 9.1m 10–5
1000=
0.75 (1– m)
Class3 spr tr1000spi
D1. 98 e8m 10–5
1000=
0.75 (1– m)
where
Dspr =absolutevalueoftherelaxationlossesoftheprestress
spi =absolutevalueoftheinitialprestress
=spm0forpost-tensioning (seeSection11.3.2)
=maximumtensilestressappliedtothetendonminustheimmediatelossesoccurringduringthestressingprocessforpre-tensioning (seeSection11.3.3)
BS EN 1992-1-1 3.3.2(4)
BS EN 1992-1-1 3.3.2(5)
BS EN 1992-1-1 3.3.2(6)
BS EN 1992-1-1 3.3.2(7)
3.3.1
16
t =timeaftertensioning(inhours) μ =spiIfpk,wherefpkisthecharacteristicvalueofthetensilestrengthofthe
prestressingsteel r1000 =valueofrelaxationloss(%),at1000hoursaftertensioningandatamean
temperatureof20°C
The long-term (final) values of the relaxation losses may be estimated from t = 500,000hours.
Relaxationlossesareverysensitivetotemperatureofthesteelwhereheattreatmentisapplied(e.g.bysteam)(seeBSEN1992-1-1Cl.10.3.2.1).Otherwisewherethetemperatureisgreaterthan50°C,therelaxationlossesshouldbeverified.
Table 3.5Relaxation losses based on using Expressions (3.28 to 3.30) in BS EN 1992-1-1
Class r1000 (%) μ = spi/fpkt (hours) Dspr/spi%
1 8 0.80 500,000 23.3
0.76 21.5
0.72 19.8
0.68 18.2
0.64 16.8
0.60 15.5
2 2.5 0.80 6.1
0.76 5.1
0.72 4.3
0.68 3.6
0.66 3.0
0.60 2.5
3 4 0.80 12.1
0.76 10.6
0.72 9.3
0.68 8.1
0.64 7.1
0.60 6.2
Relaxation lossesaresensitivetovariations instress levelsovertimeandcanthereforebereduced by taking into consideration of other time-dependent losses occurring within thestructure at the same time (such as creep and shrinkage). Previous UK practice is to basedesignontherelaxationlossof1000hourswithoutconsideringtheinteractionwithcreepandshrinkage.
BS EN 1992-1-1 3.3.2(8)
BS EN 1992-1-1 3.3.2(9)
17
Durabilityandcover
Durability and cover
General
A durable structure shall meet the requirements of serviceability, strength and stabilitythroughout its design working life, without significant loss of utility or excessive unforeseenmaintenance.
Inordertoachievetherequireddesignworkinglifeofthestructure,adequatemeasuresshallbetakentoprotecteachstructuralelementagainsttherelevantenvironmentalactions.Exposureconditionsarechemicalandphysicalconditionstowhichthestructureisexposedinadditiontomechanicalactions.
Requirements of durability should be considered at all stages of design and construction,includingtheselectionofmaterials,constructiondetails,executionandqualitycontrol.
Half-jointsshouldnotbeusedinbridgesunlessthereareadequateprovisionsforinspectionandmaintenance. Water penetration or the possibility of leakage from the carriageway intothe inside of voided structures should be considered in the design. For concrete surfacesprotectedbywaterproofingtheexposureclassis XC3 .
Where de-icing salt is used, all exposed concrete surfaces within 10m of the carriagewayhorizontally or within 5m above the carriageway should be considered as being directlyaffected by de-icing salts. Top surfaces of supports under expansion joints should also beconsideredasbeingdirectlyaffectedbyde-icingsalts.Theexposureclassesforsurfacesdirectlyaffectedbyde-icingslatsare XD3 and XF2 or XF4 asappropriate.
Adequatecoverisrequiredtoensuresafetransmissionofbondforces(seeSection4.2)andprotectionofsteelagainstcorrosion(seeSections4.3and4.4).
The concrete cover to reinforcement is the distance from the outer surface of thereinforcementtothenearestconcretesurface.Drawingsshouldspecifythenominalcover.Asillustrated in Figure 4.1, the nominal cover should satisfy the minimum requirements inrespectofbondanddurability,andallowforthedeviationtobeexpectedinexecution(seeSection4.5).
Figure 4.1Determination
of cover
Nominalcover,cnom
Minimumcover,cmin
(forbond,cmin,bor
durabilitycmin,dur)
Designallowancefor
deviation,Dcdev
BS EN 1992-1-14.1
BS EN 1992-1-1 4.3(1), 4.2(1)
BS EN 1992-1-1 4.3(2)
BS EN 1992-1-1 4.4.1.2(1)
BS EN 1992-2 4.2(106) & NA
BS EN 1992-1-1 4.4.1.3(3)
BS EN 1992-2 4.2(104), (105) & NA, PD 6687-2 5.1
4
4.1
18
Cover for bond, cmin,b
Inordertotransmitbondforcessafelyandtoensureadequatecompaction,theminimumcovershouldnotbelessthancmin,binTable4.1.
Table 4.1Minimum cover, cmin,b, requirements for bond
Reinforcement type and arrangement cmin,b
Individual bars Diameterofbar,f
Bundled bars Equivalentdiameterofbars,fn
Post-tensioned circular ducts Diameterofductor80mmwhicheverissmaller
Post-tensioned rectangular ducts Smallerdimensionorhalfgreaterdimensionwhicheverisgreater,butnotmorethan80mm
Pre-tensioned strand or wire 1.5timesthediameter
Pre-tensioned indented wire 2.5timesthediameter
Cover for durability, cmin,dur
Environmental conditions are classified according toTable 4.2, which is based on BS 8500.ConcretecompositionandminimumcoversrequiredfordurabilityindifferentenvironmentalconditionsaresetoutinTable4.3,derivedfromBS8500[8].Thesetablesgiverecommendationsfornormalweightconcreteusingmaximumaggregatesizeof20mmforselectedexposureclassesandcovertoreinforcement.
InaccordancewithBS8500 ,specialattentionshouldbegiventotheconcretecompositionand aggregates, when considering freeze/thaw attack, chemical attack or abrasionresistance.
Table 4.2Exposure Classes
Class Class description Informative example applicable to the United Kingdom
No risk of corrosion or attack (X0 class)
X0 Forconcretewithoutreinforcementorembeddedmetalallexposuresexceptwherethereisfreeze/thaw,abrasionorchemicalattack.
Unreinforcedconcretesurfacesinsidestructures.UnreinforcedconcretecompletelyburiedinsoilclassedasAC–1andwithhydraulicgradientnotgreaterthan5.Unreinforcedconcretepermanentlysubmergedinnon-aggressivewater.Unreinforcedconcreteincyclicwetanddryconditionsnotsubjecttoabrasion,freezingorchemicalattack.Note:Forreinforcedconcrete,useatleastXC1.
Corrosion induced by carbonation (XC classes)a (Where concrete containing reinforcement or other embedded metal is exposed to air and moisture)
XC1 Dryorpermanentlywet. Reinforcedandprestressedconcretesurfacesinsideenclosedstructuresexceptareasofstructureswithhighhumidity.Reinforcedandprestressedconcretesurfacespermanentlysubmergedinnon-aggressivewater.
XC2 Wet,rarelydry. ReinforcedandprestressedconcretecompletelyburiedinsoilclassedasAC–1andwithahydraulicgradientnotgreaterthan5.
XC3&
XC4
Moderatehumidityorcyclicwetanddry.
Externalreinforcedandprestressedconcretesurfacesshelteredfrom,orexposedto,directrain.Reinforcedandprestressedconcretesurfacesinsidestructureswithhighhumidity(e.g.poorlyventilated,bathrooms,kitchens).Reinforcedandprestressedconcretesurfacesexposedtoalternatewettinganddrying.Interiorconcretesurfacesofpedestriansubwaysnotsubjecttode-icingsalts,voidedsuperstructuresorcellularabutments.Reinforcedorprestressedconcretebeneathwaterproofing.
BS 8500 table A.1
4.2
4.3
BS EN 1992-1-1table 4.2
BS EN 1992-1-14.4.1.2(3) & NA
BS EN 1992-1-14.4.1.2(5) & NA
19
Durabilityandcover
Table 4.2Exposure Classes (continued)
Class Class description Informative example applicable to the United Kingdom
Corrosion induced by chlorides other than from sea water (XD classes)a (Where concrete containing reinforcement or other embedded metal is subject to contact with water containing chlorides, including de-icing salts, from sources other than from sea water)
XD1 Moderatehumidity Concretesurfacesexposedtoairbornechlorides.Reinforcedandprestressedconcretewallandstructuresupportsmorethan10mhorizontallyfromacarriageway.Bridgedecksoffitsmorethan5mverticallyabovethecarriageway.Partsofstructuresexposedtooccasionalorslightchlorideconditions.
XD2 Wet,rarelydry. Reinforcedandprestressedconcretesurfacestotallyimmersedinwatercontainingchloridesb.Buriedhighwaystructuresmorethan1mbelowadjacentcarriageway.
XD3 Cyclicwetanddry. Reinforcedandprestressedconcretesurfacesdirectlyaffectedbyde-icingsaltsorspraycontainingde-icingsalts(e.g.walls;abutmentsandcolumnswithin10mofthecarriageway;parapetedgebeamsandburiedstructureslessthan1mbelowcarriagewaylevel,pavementsandcarparkslabs).
Corrosion induced by chlorides from sea water (XS classes)a (Where concrete containing reinforcement or other embedded metal is subject to contact with chlorides from sea water or air carrying salt originating from sea water)
XS1 Exposedtoairbornesaltbutnotindirectcontactwithseawater.
Externalreinforcedandprestressedconcretesurfacesincoastalareas.
XS2 Permanentlysubmerged. Reinforcedandprestressedconcretecompletelysubmergedandremainingsaturated,e.g.concretebelowmid-tidelevelb.
XS3 Tidal,splashandsprayzones. Reinforcedandprestressedconcretesurfacesintheuppertidalzonesandthesplashandsprayzonesc.
Freeze/thaw attack (XF classes) (Where concrete is exposed to significant attack from freeze/thaw cycles whilst wet)
XF1 Moderatewatersaturationwithoutde-icingagent.
Verticalconcretesurfacessuchasfacadesandcolumnsexposedtorainandfreezing.Non-verticalconcretesurfacesnothighlysaturated,butexposedtofreezingandtorainorwater.
XF2 Moderatewatersaturationwithde-icingagent.
Concretesurfacessuchaspartsofbridges,whichwouldotherwisebeclassifiedasXF1butwhichareexposedtode-icingsaltseitherdirectlyorassprayorrun-off.
XF3 Highwatersaturationwithoutde-icingagent.
Horizontalconcretesurfaces,suchaspartsofbuildings,wherewateraccumulatesandwhichareexposedtofreezing.Concretesurfacessubjectedtofrequentsplashingwithwaterandexposedtofreezing.
XF4 Highwatersaturationwithde-icingagentorseawaterd.
Horizontalconcretesurfaces,suchasroadsandpavements,exposedtofreezingandtode-icingsaltseitherdirectlyorassprayorrun-off.Concretesurfacessubjectedtofrequentsplashingwithwatercontainingde-icingagentsandexposedtofreezing.
Chemical attack (ACEC classes) (Where concrete is exposed to chemical attack. Note: BS 8500-1 refers to ACEC classes rather than XA classes used in BS EN 206-1)
RefertoSection4.4
Key
a Themoistureconditionrelatestothatintheconcretecovertoreinforcementorotherembeddedmetalbut,inmanycases,conditionsintheconcretecovercanbetakenasbeingthatofthesurroundingenvironment.Thismightnotbethecaseifthereisabarrierbetweentheconcreteanditsenvironment.
b Reinforcedandprestressedconcreteelements,whereonesurfaceisimmersedinwatercontainingchloridesandanotherisexposedtoair,arepotentiallyamoreseverecondition,especiallywherethedrysideisatahighambienttemperature.Specialistadviceshouldbesoughtwherenecessary,todevelopaspecificationthatisappropriatetotheactualconditionslikelytobeencountered.
c ExposureXS3coversarangeofconditions.Themostextremeconditionsareinthesprayzone.TheleastextremeisinthetidalzonewhereconditionscanbesimilartothoseinXS2.TherecommendationsgiventakeintoaccountthemostextremeUKconditionswithinthisclass.
d ItisnotnormallynecessarytoclassifyintheXF4exposureclassthosepartsofstructureslocatedintheUnitedKingdomwhichareinfrequentcontactwiththesea.
20
Table 4.3Selecteda recommendations for normal-weight reinforced concrete quality for combined exposure classes and cover to reinforcement
Exposure conditions Cement/ combina-tion desig-nationsb
Minimum strength classc, maximum w/c ratio, minimum cement or combination
Typical example
Primary Secondary At least 50-year working life
Nominal cover to reinforcementd
15 +Dcdev 20 +Dcdev 25 +Dcdev 30 +Dcdev 35 +Dcdev 40 +Dcdev 45 +Dcdev
Internalelementsorpermanentlywetelements
XC1 – AllC20/25,0.70,240orRC20/25
<<< <<< <<< <<< <<< <<<
BuriedconcreteinAC–1groundconditionse
XC2 AC–1 All – –C25/30,0.65,260orRC25/30
<<< <<< <<< <<<
Verticalsurfaceprotectedfromdirectrainfall
XC3/4
– AllexceptIVB-V
–C40/50,0.45,340orRC40/50
C30/37,0.55,300orRC30/37
C28/35,0.60,280orRC28/35
C25/30,0.65,260orRC25/30
<<< <<<
Verticalsurfaceexposedtorainandfreezing
XF1 AllexceptIVB-V
–C40/50,0.45,340orRC40/50
C30/37,0.55,300orRC30/37
C28/35,0.60,280orRC28/35
<<< <<< <<<
Exposedhorizontalsurfaces
XF3 AllexceptIVB-V
–C40/50,0.45,340gorRC40/50XFg
<<< <<< <<< <<< <<<
XF3(airentrained)
AllexceptIVB-V
– – C30/37,0.55,300g,h
C28/35,0.60,280g,horPAV2
C25/30,0.60,280g, h,jorPAV1
<<< <<<
Elementssubjecttoairbornechlorides
XD1f XF1 All – – C40/50,0.45,360
C32/40,0.55,320
C28/35,0.60,300 <<< <<<
Exposedverticalsurfacesnearcoast
XS1f
XF1
CEMI,IIA,IIB-S,SRPC
– – – SeeBS8500 C35/45,0.45,360
C32/40,0.50,340 <<<
IIB-V,IIIA – – – SeeBS8500
C32/40,0.45,360
C28/35,0.50,340
C25/30,0.55,320
– IIIB – – – C32/40,0.40,380
C25/30,0.50,340
C25/30,0.50,340
C25/30,0.55,320
Exposedhoriz.surfacesnearcoast
XF3orXF4
CEMI,IIA,IIB-S,SRPC
– – – SeeBS8500 C40/50,0.45,360g <<< <<<
Elementssubmergedinwatercontainingchlorides
XD2orXS2f –
CEMI,IIA,IIB-S,SRPC
– – – C40/50,0.40,380
C32/40,0.50,340
C28/35,0.55,320 <<<
IIB-V,IIIA – – – C35/45,0.40,380
C28/35,0.50,340
C25/30,0.55,320 <<<
IIIB,IVB-V – – – C32/40,0.40,380
C25/30,0.50,340
C20/25,0.55,320 <<<
Elementssubjecttomoderatewatersaturationwithde-icingagentandfreezing
XD3f
XF2
IIB-V,IIIA – – – – – C35/45,0.40,380
C32/40,0.45,360
CEMI,IIA,IIB-S,SRPC
– – – – – SeeBS8500 C40/50,0.40,380
IIIB,IVB-V – – – – – C32/40,0.40,380
C32/400.45,360
Elementssubjecttowatersaturationwithde-icingagentandfreezing
XF4k IIB-V,IIIA – – – – – C40/50,0.45,380g
C40/50,0.45,360g
XF4(airentrained)
CEMI,IIA,IIB-S,SRPC
– – – – – SeeBS8500 C28/35,0.40,380g
IIB-V,IIIA – – – – – C28/35,0.40,380g,h
C28/350.45,360g,h
Elementsintidal,splashandsprayzones
XS3 –
CEMI,IIA,IIB-S,SRPC
– – – – – – SeeBS8500
IIB-V,IIIA – – – – – C35/45,0.40,380
C32/40,0.45,360
IIIB,IVB-V – – – – – C32/40,0.40,380
C28/35,0.45,360
Key
aThistablecomprisesaselectionofcommonexposureclasscombinations.Requirementsforothersetsofexposureclasses,e.g.XD2,XS2andXS3shouldbederivedfromBS8500–1:2006,AnnexA.
bSeeTable4.4(CEMIisPortlandcement,IIAtoIVBarecement/combinations.)
cForprestressedconcretetheminimumstrengthclassshouldbeC28/35.
dDcdevisanallowancefordeviations.
21
Durabilityandcover
for either at least a 50-year or 100-year intended working life and 20 mm maximum aggregate size
content (kg/m3), and equivalent designated concrete where applicable
At least 100-year working life
Nominal cover to reinforcementd
50 +Dcdev 15 +Dcdev 25 +Dcdev 30 +Dcdev 35 +Dcdev 40 +Dcdev 45 +Dcdev 50 +Dcdev 55 +Dcdev 60 +Dcdev 65 +Dcdev
<<<C20/25,0.70,240RC20/25
<<< <<< <<< <<< <<< <<< <<< <<< <<<
<<< –C25/30,0.65,260RC25/30
<<< <<< <<< <<< <<< <<< <<< <<<
<<< – –C40/50,0.45,340RC40/50
C35/45,0.50,320RC35/45
C30/37,0.55,300RC30/37
C28/35,0.60,280RC28/35
C25/30,0.65,260RC25/30
<<< <<< <<<
<<< – –C40/50,0.45,340RC40/50
C35/45,0.50,320RC35/45
C30/37,0.55,300RC30/37
C28/35,0.60,280RC28/35
<<< <<< <<< <<<
<<< – –
C40/50,0.45,340g
RC40/50 <<< <<< <<< <<< <<< <<< <<<
<<< – – – C35/45,0.50,320g,h
C30/37,0.55,300g,h
C28/35,0.60,280g,h
orPAV2
C25/300.60,280g,h,j
orPAV1<<< <<< <<<
<<< – – C45/55,
0.40,380C40/50,0.45,360
C35/45,0.50,340
C32/40,0.55,320
C28/35,0.60,300 <<< <<< <<<
<<< – – – – – SeeBS8500
C40/50,0.40,380
C35/45,0.45,360 <<< <<<
<<< – – – C35/45,0.40,380
C32/40,0.45,360
C28/35,0.50,340
C25/30,0.55,320 <<< <<< <<<
<<< – – – C35/45,0.45,360
C30/37,0.50,340
C28/35,0.55,320
C25/30,0.55,320 <<< <<< <<<
<<< – – – – – SeeBS8500 C40/50,0.40,380g <<< <<< <<<
<<< – – – – C35/45,0.45,360
C32/40,0.50,340
C28/35,0.55,320 <<< <<< <<<
<<< – – – – C32/40,0.45,360
C28/35,0.50,340
C25/30,0.55,320 <<< <<< <<<
<<< – – – – C28/35,0.45,360
C25/30,0.50,340
C20/25,0.55,320 <<< <<< <<<
C32/40,0.50,340
– – – – – SeeBS8500 C35/45,0.40,380
C32/40,0.45,360
C28/35,0.50,340
C25/30,0.55320
C35/45,0.45,360
– – – – – – – SeeBS8500 C40/50,0.40,380
C35/45,0.45,360
C32/40,0.50,340
– – – – – C32/40,0.40,380
C28/35,0.45,360
C25/30,0.50,340 <<< <<<
C40/50,0.45,340
– – – – – SeeBS8500 C40/50,0.40,380g
C40/50,0.45,360g
C40/50,0.45,340g
C40/50,0.45,340g
C28/35,0.45,360g – – – – – – – See
BS8500C28/35,0.40,380g
C28/35,0.45,360g
C28/35,0.50,340g,h – – – – – SeeBS8500 C28/35,
0.40,380g,hC28/35,0.45,360g,h
C28/35,0.50,340g,h
C28/35,0.55,320g,h
C40/50,0.40,380
– – – – – – – – SeeBS8500 C40/50,0.40,380
C28/35,0.50,340
– – – – – SeeBS8500 C35/45,0.40,380
C32/40,0.45,360
C28/35,0.50,340
C25/30,0.55,320
C25/30,0.50,340
– – – – – C32/40,0.40,380
C28/35,0.45,360
C25/30,0.50,340 <<< <<<
e Forsectionslessthan140mmthickrefertoBS8500.
f AlsoadequateforexposureclassXC3/4.
g Freeze/thawresistingaggregatesshouldbespecified.
h Airentrainedconcreteisrequired.
j Thisoptionmaynotbesuitableforareassubjecttosevereabrasion.
k Notrecommendedforpavementsandhardstandings–seeBS8500-1,A.4.3.
– Notrecommended
<<< Indicatesthatconcretequalityincelltotheleftshouldnotbereduced
22
Table 4.4Cement and combination typea
Broad designationb
Composition Cement/combination types (BS 8500)
CEM I Portlandcement CEMI
SRPC Sulfate-resistingPortlandcement SRPC
IIA Portlandcementwith6–20%flyash,groundgranulatedblastfurnaceslag,limestone,or6–10%silicafumec
CEMII/A-L,CEMII/A-LL,CIIA-L,CIIA-LL,CEMII/A-S,CIIA-S,CEMII/A-V,CIIA-V,CEMII/A–D
IIB-S Portlandcementwith21–35%groundgranulatedblastfurnaceslag
CEMII/B-S,CIIB-S
IIB-V Portlandcementwith21–35%flyash CEMII/B-V,CIIB-V
IIB+SR Portlandcementwith25–35%flyash CEMII/B-V+SR,CIIB-V+SR
IIIAd, e Portlandcementwith36–65%groundgranulatedblastfurnaceslag
CEMIII/A,CIIIA
IIIA+SRe Portlandcementwith36–65%groundgranulatedblastfurnaceslagwithadditionalrequirementsthatenhancesulfateresistance
CEMIII/A+SRf,CIII/A+SRf,CIIIA+SR
IIIBe, g Portlandcementwith66–80%groundgranulatedblastfurnaceslag
CEMIII/B,CIIIB
IIIB+SRe Portlandcementwith66–80%groundgranulatedblastfurnaceslagwithadditionalrequirementsthatenhancesulfateresistance
CEMIII/B+SRf,CIIIB+SRf
IVB-V Portlandcementwith36–55%flyash CEMIV/B(V),CIVB
Keya Thereareanumberofcementsandcombinationsnotlistedinthistablethatmaybespecifiedfor
certainspecialistapplications.SeeBRESpecialDigest[19]forthesulfate-resistingcharacteristicsofothercementsandcombinations.
b Theuseofthesebroaddesignationsissufficientformostapplications.Whereamorelimitedrangeofcementorcombinationstypesisrequired,selectfromthenotationsgiveninBS8500–2:2006,Table1.
c WhenIIAorIIA–Disspecified,CEMIandsilicafumemaybecombinedintheconcretemixerusingthek-valueconcept;seeBSEN206–1:2000,Cl.5.2.5.2.3.
d WhereIIIAisspecified,IIIA+SRmaybeused.
e Inclusiveoflowearlystrengthoption(seeBSEN197–4andthe‘L’classesinBS8500–2:2006,TableA.1).
f ‘+SR’indicatesadditionalrestrictionsrelatedtosulfateresistance.SeeBS8500–2:2006,Table1,footnoteD.
g WhereIIIBisspecified,IIIB+SRmaybeused.
Chemical attack
Whereplainorreinforcedconcreteisincontactwiththeground,furtherchecksarerequiredtoachievedurability.Anaggressivechemicalenvironmentforconcreteclass(ACECclass)shouldbeassessedforthesite.BRE Special Digest 1[19]givesguidanceontheassessmentoftheACECclassandthis isnormallycarriedoutaspartoftheinterpretivereportingforaground investigation. Knowing theACEC class, a design chemical class (DC class) can beobtainedfromTable4.5.Ingeneral,fullyburiedconcreteintheUKneednotbedesignedtobefreeze-thawresisting.
For designated concretes, an appropriate foundation concrete (FND designation) can beselectedusingTable4.6.AnFNDconcretehasthestrengthclassofC25/30.Whereahigherstrengthisrequired,eitherforitsstrengthorwherethefoundationisclassifiedasXD2orXD3, a designed concrete should be specified. For designed concretes, the concreteproducershouldbeadvisedoftheDC–class.
BS 8500 table A.6
4.4
23
Durabilityandcover
4.5 Dcdev and other allowances
Tocalculatethenominalcover,cnom,anadditiontotheminimumcovershallbemadeindesignto allow for the deviation (Dcdev). In the UK the recommended value is 10mm. In certainsituationstheaccepteddeviationandhenceallowanceDcdevmaybereduced:
■ Wherefabricationissubjectedtoaqualityassurancesystem,inwhichthemonitoringincludesmeasurementsoftheconcretecover,theallowanceindesignfordeviationDcdevmaybereduced:10mm≥Dcdev≥5mm
■ Whereitcanbeassuredthataveryaccuratemeasurementdeviceisusedformonitoring,andnon-conformingmembersarerejected(e.g.precastelements),theallowanceindesignfordeviationDcdevmaybereduced:10mm≥Dcdev≥0mm
DcdevisrecognisedinBS8500asDc.
Theminimumcoverforconcretecastonpreparedground(includingblinding)is 40mm andthatforconcretecastdirectlyagainstsoilis 65mm.
Forunevensurfaces(e.g.exposedaggregate)theminimumcovershouldbeincreasedbyatleast5mm.
Table 4.5Selection of the DC–class and the number of additional protection measures (APMs) where the hydrostatic head of groundwater is not more than five times the section width a, b, c, d, e
ACEC-class (aggressive chemical environment for concrete class)
Intended working life
At least 50 years At least 100 years
AC–1s, AC–1 DC–1 DC–1
AC–2s, AC–Z DC–2 DC–2
AC–2z DC–2z DC–2z
AC–3s DC–3 DC–3
AC–3z DC–3z DC–3z
AC–3 DC–3 RefertoBS8500
AC–4s DC–4 DC–4
AC–4z DC–4z DC–4z
AC–4 DC–4 RefertoBS8500
AC–4ms DC–4m DC4m
AC–4m DC–4m RefertoBS8500
AC–5 DC–4f DC–4f
AC–5z DC–4zf DC–4z/1f
AC–5m DC–4mf DC–4mf
Keya Wherethehydrostaticheadofgroundwaterisgreaterthanfivetimesthesectionwidth,refertoBS
8500.
b ForguidanceonprecastproductsseeSpecialDigest1[19].
c ForstructuralperformanceoutsidethesevaluesrefertoBS8500.
d Forsectionwidths<140mmrefertoBS8500.
e Whereanysurfaceattackisnotacceptablee.g.withfrictionpiles,refertoBS8500.
f ThisshouldincludeAPM3(surfaceprotection),wherepracticable,asoneoftheAPMs;refertoBS8500.
BS EN 1992-1-1 4.4.1.3(1)&(3) & NA
BS EN 1992-1-1 4.4.1.3(4) & NA
BS EN 1992-1-1 4.4.1.2(11)
BS 8500 table A.9
24
BS EN 1992-2 4.4.1.2(114)
BS 8500 table A.1
BS EN 1992-2 4.4.1.2(115)
Table 4.6Guidance on selecting designated concrete for reinforced concrete foundations
DC-Class Appropriate designated concrete
DC–1 RC 25/30
DC–2 FND2
DC–2z FND2z
DC–3 FND3
DC–3z FND3z
DC–4 FND4
DC–4z FND4z
DC–4m FND4m
NoteStrength class for all FND concrete is C25/30.
Bare concrete decks of road bridges, without waterproofing or surfacing, should be classified as Abrasion Class XM2.
Where a concrete surface is subject to abrasion caused by ice or solid transportation in running water, the cover should be increased by a minimum of 10 mm.
25
Structuralanalysis
Structural analysis
General
Thepurposeofstructuralanalysis istoestablishthedistributionofeither internal forcesandmomentsorstresses,strainsanddisplacementsoverthewholeorpartofastructure.Additionallocalanalysisshallbecarriedoutwherenecessary.
Whendesigningabridgedeckslabofboxbeamorbeamandslabconstruction,itisnecessarytoconsider,inadditiontooverallglobaleffects,thelocaleffectsinducedinthetopslabbywheelloads.CurrentpracticeistouseelasticanalysisandoftenassumefullfixityattheslabandwebjunctionsanduseeitherPucher’sinfluencesurfaces,Westergaard’sequations,orFEanalysis.
Idealisation of the structure
Definitions
Forbridgestructuresthefollowingcanbeapplied:
■ Abeamisamemberforwhichthespanisnotlessthanthreetimesitsdepth.Ifnot,itisadeepbeam.
■ Aslabisamemberforwhichtheminimumpaneldimensionisnotlessthanfivetimestheoverallthickness.
■ Aone-wayspanningslabhaseithertwoapproximatelyparallelunsupportededgesor,whensupportedonfouredges,theratioofthelongertoshorterspanexceeds2.0.
■ Acolumnisamemberforwhichthesectiondepthdoesnotexceedfourtimesitswidthandtheheightisatleastthreetimesthesectiondepth.Ifnot,itisawall.
Effective flange width
Theeffectivewidthofaflange,beff,shouldbebasedonthedistance,l0,betweenpointsofzeromomentsasshowninFigure5.1anddefinedinFigure5.2.
beff=bw+beff,1+beff,2
where beff,1 = (0.2b1+0.1l0)but≤0.2l0and≤b1 beff,2 = tobecalculatedinasimilarmannertobeff,1butb2shouldbesubstituted forb1intheabove
l1 l2 l3
l0=0.85l1 l0=0.15(l1+l2) l0=0.7l2 l0=0.15l2+l3
Figure 5.1Elevation showing definition of l0 for calculation of flange width
BS EN 1992-1-15.1.1(1)
BS EN 1992-1-1 5.3.1
BS EN 1992-1-1 5.3.2.1(2)&(3)
BS EN 1992-1-1fig. 5.2
5
5.1
5.2
5.2.1
5.2.2
26
Effective span
Theeffectivespan,leff,ofamembershouldbecalculatedasfollows:leff=ln+a1+a2
where ln=cleardistancebetweenthefacesofthesupports;valuesfora1anda2,ateachendof
thespan,maybedeterminedfromtheappropriateaivaluesinFigure5.3wheretisthewidthofthesupportingelementasshown.
beff
beff,1 beff,2
bw
bw
b1 b1 b2 b2
b
Figure 5.2Section showing effective flange width parameters
h
ln
ai=MIN(ah;at)
a) Non-continuous members b) Continuous members
ai=MIN(ah;at)leff
t
t
t
t
h
ln
ln
ai=MIN(ah;at)
c) Supports considered fully restrained d) Bearing provided
leff
ai=MIN(ah;at)
e) Cantilever
leff
leff
leff
ai ln
cL
ln
h
h
Figure 5.3Effective span, leff, for different support conditions
BS EN 1992-1-1fig. 5.3
BS EN 1992-1-1fig. 5.4
BS EN 1992-1-1 5.3.2.2(1)
5.2.3
27
Structuralanalysis
Methods of analysis
Ultimate limit states (ULS)
Thetypeofanalysisshouldbeappropriatetotheproblembeingconsidered.Thefollowingarecommonlyused:linearelasticanalysis,linearelasticanalysiswithlimitedredistribution,andplasticanalysis.
Fordeterminationoftheactioneffects,linearelasticanalysismaybecarriedoutassuming:
■ Uncrackedcross-sections.■ Linearstress–strainrelationships.■ Theuseofmeanvaluesofelasticmodulus.
Ifa linearelasticanalysiswith limitedredistribution isundertaken,shearsandreactionsused in the design should be taken as those either prior to redistribution or afterredistribution,whicheverisgreater.
Incontinuousbeamsorslabswhich:
■ Arepredominantlysubjecttoflexure■ Havetheratiooflengthsofadjacentspansintherangeof0.5to2.0
redistributionofbendingmomentmaybecarriedoutwithoutexplicitcheckontherotationcapacityprovidedthat:
d≥ 0.44 + 1.25(0.6+0.0014/ecu2) xu/d forfck≤50MPad≥ 0.54 + 1.25(0.6+0.0014/ecu2) xu/d forfck>50MPad≥ 0.85whereClassBandClassCreinforcementisused
where d = theratiooftheredistributedmomenttothemomentinthelinearelasticanalysis xu= thedepthoftheneutralaxisattheultimatelimitstateafterredistribution d = theeffectivedepthofthesection
Redistributionshouldnotbecarriedoutincircumstanceswheretherotationcapacitycannotbedefinedwithconfidence(e.g.incurvedandorskewedbridges).
Itisrecommendedthatmomentredistributionisnotusedforsectionsdeeperthan1.2munlessarigorousanalysisofrotationcapacityisundertaken.
Thefollowingrulesmaybeusedforsolidconcreteslabswithfck≤50MPa.
d≥ 0.4 + 1.0 xu/d≥0.7wherethereinforcementisClassBorClassC
NoredistributionisallowedforClassAreinforcement.
Whereused,plasticanalysisshouldbebasedeitheronstatic(lowerbound)orkinematic(upperbound) methods.The ductility of the critical sections should be sufficient for the envisagedmechanism to be formed.The required ductility may be deemed to be satisfied if all of thefollowingarefulfilled:
■ xu/d≤0.15forfck≤50MPa■ xu/d≤0.10forfck≥50MPa■ ReinforcementiseitherClassBorC;and■ Ratioofthemomentsatinternalsupportstothemomentsinthespanisbetween0.5and2.0.
Forsolidslabsxu/d≤0.25maybeusedwhenfck≤50MPa.
BS EN 1992-1-1 5.1.1(6)
BS EN 1992-1-1 5.4(2)
BS EN 1992-2 5.5(104) & NA
PD 6687-26.4
BS EN 1992-1-15.6.1(3) & (2)
BS EN 1992-25.6.2(102)
BS EN 1992-2 5.5(104)
PD 6687-2 6.6
BS EN 1992-2 5.5 (105)
5.3
5.3.1
28
Non-linearanalysisshouldbeundertakenusingmodel factorsandmaterialmodels,whichgiveresultsthaterronthesafeside.Typically,thismaybeachievedbyusingdesignmaterialproperties and applying design actions. However, in some situations, underestimatingstiffnessthroughtheuseofdesignpropertiescanleadtounsaferesults.Suchsituationscaninclude cases where indirect actions such as imposed deformations are significant, caseswhere the failure load is associated with a local brittle failure mode, and cases where theeffectoftensionstiffeningisunfavourable.Insuchsituations,sensitivityanalysesshouldbeundertaken to investigate the effect of variations in material properties, including spatialvariations,toprovideconfidencethattheresultsoftheanalysisdoerronthesafeside.
Fornon-linearanalysisthatconsidersonlydirectandflexuraleffects,referencemaybemadetoBSEN1992-2,Cl.5.8.6.Suchanalysisshouldaccountfortheeffectsoflong-termloading.EffectsnotconsidereddirectlyintheanalysisshouldbeconsideredseparatelyinaccordancewithSections6to11.
Non-linearanalysisthatdeterminesshearandtorsionalstrengthdirectlyhasnotyetreachedastagewhereitcanbefullycodified.Particularanalysesmaybeusedwhentheyhavebeenshownbycomparisonwithteststogivereliableresults,withtheagreementoftheNationalAuthority.
Serviceability limit states (SLS)
Linearelasticanalysismaybecarriedoutassuming:
■ Uncrackedcross-sections.■ Linearstress–strainrelationships.■ Theuseofmeanvaluesofelasticmodulus.
The moments derived from elastic analysis should not be redistributed but a gradualevolutionofcrackingshouldbeconsidered,whichrequiresanon-linearanalysisallowingfortheeffectofcrackingandtensionstiffening.Un-crackedglobalanalysisinaccordancewithBS EN 1992-1-1 Cl. 5.4 (2) may always be used as a conservative alternative to suchconsiderations.
General note
Regardlessofthemethodofanalysisused,thefollowingapply.
■ Whereabeamorslabismonolithicwithitssupports,thecriticaldesignmomentatthesupportmaybetakenasthatatthefaceofthesupport.Thedesignmomentandreactiontransferredtothesupportingelement(e.g.column,wall,etc.)shouldbegenerallytakenasthegreateroftheelasticorredistributedvalues.Themomentatthefaceofthesupportshouldnotbetakenaslessthan 65% ofthefullfixedendmoment.
■ Whereabeamorslabiscontinuousoverasupportwhichisconsideredtoprovidenorestrainttorotation(e.g.overwalls)andtheanalysisassumespointsupport,thedesignsupportmomentcalculatedonthebasisofaspanequaltothecentre-to-centredistancebetweensupports,maybereducedbyanamountDMEdasfollows:
DMEd=FEd,supt/8
where FEd,sup=designsupportreaction t =breadthofbearing
BS EN 1992-1-1 5.4
BS EN 1992-2 5.7 (105) & NA
5.3.2
5.3.3
BS EN 1992-1-1 5.3.2.2(3)
BS EN 1992-1-1 5.3.2.2(104)
29
Structuralanalysis
Loading
Combinations of actions
Thefollowingcombinationsofactionsshouldbeusedwhereappropriate.
Ultimate Limit State Persistent or transient design situations:gGGk + gp P + gQ,1 Qk,1 + S gQ,ic0,i Qk,i i >1
Accidental design situations:Gk + P + Ad + c1,1Qk,1 + S c2,i Qk,i i >1
Note:c2,1maybesubstitutedforc1,1dependingontheaccidentaldesignsituation.
Serviceability Limit StateCharacteristic combination of actions:
Gk + P + Qk,1 + S c0,i Qk,i i >1
Tobeusedforstresslimitationcheckforconcreteandsteel.
Frequent combination of actions:Gk + P + c1,1 Qk,1+ S c2,i
Qk,i i >1
Tobeusedfordecompressioncheckorcrackwidthcheckforprestressedconcretewithbondedtendons.
Quasi-permanent combination of actions:Gk + P + S c2,i
Qk,i i >1
Tobeusedforcrackwidthcheckforreinforcedconcreteandprestressedconcretewithoutbondedtendonsanddeformationcheck.
TermsCombinationvalueofavariableaction:c0QFrequentvalueofavariableaction:c1QQuasi-permanentvalueofavariableaction:c2Q
Load casesInconsideringthecombinationsofactions(seeSection6andAnnexA2ofBSEN1990)therelevantloadcasesshallbeconsideredtoenablethecriticaldesignconditionstobeestablishedatallsections,withinthestructureorpartofthestructureconsidered.
Geometrical imperfections
General
Theunfavourableeffectsofpossibledeviationsinthegeometryofthestructureandthepositionofloadsshallbetakenintoaccountintheanalysisofmembersandstructures.
Imperfections shall be taken into account in ultimate limit states in persistent and accidentaldesignsituations.
BS EN 1992-1-1 5.2(1)
BS EN 1990 6.4.3
BS EN 1992-2 5.1.3
BS EN 1992-1-1 5.2(2)
5.4
5.4.1
5.5
5.5.1
30
Imperfections and global analysis of structures
Imperfectionsmayberepresentedbyaninclinationyigivenby:
y1=(1/200) ah
where ah = 2/l0.5≤1.0 l = lengthorheightinmetres
Forisolatedmemberstheeffectoftheimperfectionsmayberepresentedasaneccentricityorbyatransverseforce.
Theeccentricity,ei,givenbyei=yil0/2wherel0istheeffectivelength
Thetransverseforceisappliedinthepositionthatgivesmaximummoment.
Hi=y1Nk
where Hi= actionappliedatthatlevel N = axialload k = 1.0forunbracedmembers(seeFigure5.4a) = 2.0forbracedmembers(seeFigure5.4b)
Forarchbridges,theshapeofimperfectionsinthehorizontalandverticalplanesshouldbebasedontheshapeofthefirsthorizontalandverticalbucklingmodeshaperespectively.Eachmodeshapemaybeidealisedbyasinusoidalprofile.Theamplitudeshouldbetakenasa=y1l/2,wherelisthehalfwavelength.
Thedispositionofimperfectionsusedinanalysisshouldreflectthebehaviourandfunctionofthestructureanditselements.Theshapeofimperfectionshouldbebasedontheanticipatedmode of buckling of the member. For example, in the case of bridge piers, an overall leanimperfectionshouldbeusedwherebucklingwillbeinaswaymode(“unbraced”conditions),whilealocaleccentricitywithinthemembershouldbeusedwherebothendsofthememberareheldinposition(“braced”conditions).
In using Expression (5.2) of Part 1-1 the eccentricity, ei, derived should be taken as theamplitude of imperfection over the half wavelength of buckling; Figure 5.5 shows theimperfectionsuitableforapierrigidlybuiltinformomentateachend.Aleanimperfectionshould however be considered in the design of the positional restraints for braced members.FurtherguidanceandbackgroundaregiveninHendyandSmith.[20]
b) Braced isolated membersa) Unbraced isolated members
ei ei
N NN N
Hi
l = l0/2 Hi l = l0
Figure 5.4Examples of the effects of geometric imperfections
BS EN 1992-2 5.2(105)
BS EN 1992-1-1 5.2(7)
BS EN 1992-1-1 Exp. (5.2)
BS EN 1992-25.2(106)
PD 6687-2 6.2
BS EN 1992-1-1fig. 5.1a
5.5.2
31
Structuralanalysis
5.6
5.6.1
PD 6687-2fig. 1
BS EN 1992-1-1 5.8.1
BS EN 1992-1-1 5.8.3.2(3)
ei eei
l0 yI
l0 = l/2e = 2ei= yI/2
b) Angular imperfectiona) Sinusoidal imperfection
Figure 5.5Imperfections for pier built in at both ends
Design moments in columns
Definitions
Bracing members
Bracing members are members that contribute to the overall stability of the structure,whereasbracedmembersdonot contributetotheoverallstabilityofthestructure.
Effective length l0Forbracedmembers:
l0=0.5l[(1+k1/(0.45+k1))(1+k2/(0.45+k2))]0.5
Forunbracedmembersl0isthelargerofeither:
l0=l[1+10k1k2/(k1+k2)]0.5orl0=l[1+k1/(1.0+k1)][1+k2/(1.0+k2)]
where l = clearheightofthecolumnbetweentheendrestraints k1,k2 = relativeflexibilitiesofrotationalrestraintsatends1and2respectively
ExamplesofdifferentbucklingmodesandcorrespondingeffectivelengthfactorsforisolatedmembersareshowninFigure5.6.PD6687-2[3]notesthattheeffectivelengthsshowndonotcovertypicalbridgecasesandprovidesadditionalexamples,whicharegiveninTable5.1.
BS EN 1992-1-1 5.8.3.2(2)PD 6687-2, 6.71
32
y
y
y
l
M
a) l0 = l b) l0 = 2l c) l0 = 0.7l d) l0 = l/2 e) l0 = l f) l/2 < l0 < l g) l0 > 2l
Figure 5.6Examples of different buckling modes and corresponding effective lengths for isolated members
Slenderness ratio, lSlendernessratiol=l0/i
where i=theradiusofgyrationoftheuncrackedconcretesection
Ignoringreinforcement:
l =3.46l0 /hforrectangularsections =4.0l0 /dforcircularsections
where h=thedepthinthedirectionunderconsideration d=thediameter
Limiting slenderness ratio llimThe limiting slenderness ratio, llim, above which second order effects should be considered,isgivenby
llim=20ABC/n0.5
where A = 1/(1+0.2hef)(ifhefisnotknownAmaybetakenas0.7) where hef = effectivecreepfactor=h(∞,t0)M0Eqp/M0Ed
h(∞,t0) = finalcreepcoefficient(seeSection3.1.2)
M0Eqp = thefirstorderbendingmomentinthequasi-permanentloadcombination(SLS)
M0Ed = thefirstorderbendingmomentindesignloadcombination(ULS)
B = (1+2w)0.5(ifwisnotknownBmaybetakenas1.1) where w = mechanicalreinforcementratio =(As/Ac)(fyd/fcd) As =totalareaoflongitudinalreinforcement
C = 1.7–rm(Ifrmisnotknown,Cmaybetakenas0.7 where rm = M01/M02,whereM01andM02arethefirstorderendmomentsatULSwith
M02numericallylargerthanM01.IfM01andM02givetensiononthesamesidethenrmispositive(andC<1.7),seeFigure5.7
rm = 1.0forunbracedmembersandbracedmembersinwhichthefirstordermomentsarecausedlargelybyimperfectionsortransverseloading
BS EN 1992-1-1 5.8.3.2(1)
BS EN 1992-1-1fig. 5.7
BS EN 1992-1-1 5.8.3.1(1) & NA
BS EN 1992-1-1 5.8.4
BS EN 1992-1-1 3.1.4(4), 3.1.4(5)
33
Structuralanalysis
Table 5.1Effective height, l0 for columns
Case Idealized column and buckling mode Restraints Effective
height l0Location Position Rotation
1
l
Top Full Fulla 0.70l
Bottom Full Fulla
2
l
Top Full None 0.85l
Bottom Full Fulla
3
l
Top Full None 1.0l
Bottom Full None
4
Elastometricbearingb
l
Top Nonec Nonec 1.3l
Bottom Full Fulla
5
l
Top None None 1.4l
Bottom Full Fulla
6
l
Top None Fulla 1.5l
Bottom Full Fulla
7
orl l
Top None None 2.3l
Bottom Full Fulld
NotesTheheightofthebearingsisnegligiblecomparedwiththatofthecolumn.
Keya Rotationalrestraintisatleast4(EI)/l,where(EI)istheflexuralrigidityofthecolumnb Mayalsobeusedwithrollerbearingsprovidedthattherollersareheldinplacebyaneffectivemeans,suchasracksc Lateralandrotationalrigidityofelastomericbearingsarenegligibled Rotationalrestraintisatleast8(EI)/l,where(EI)istheflexuralrigidityofthecolumn
PD 6687-2table 1
34
n = NEd/(Ac fcd) where NEd=designvalueofaxialforce
Note:hefmaybetakenas0ifallthefollowingconditionsaremet:■h(∞,t0) ≤2.0;■l ≤75;and■M0Ed /NEd ≥h,thedepthofthecross-sectionintherelevantdirection.
Figure 5.7Values of C
for different values of rm
a) C = 0.7, rm = 1.0 b) C = 1.7, rm = 0 c) C = 2.7, rm = – 1.0
M01=M02
M02 M02 M02
M01=–M020
Design bending moments
Non-slender columns
Whenl≤llimi.e.whennon-slender,thedesignbendingmomentinacolumnis
MEd=M02
where MEd = designmoment
M02,M01 = firstorderendmomentsatULSincludingallowancesforimperfections.M02isnumericallylargerthanM01.Attentionshouldbepaidtothesignofthebendingmoments.Iftheygivetensiononthesameside,M01andM02shouldhavethesamesign
M02 = M+eiNEd
where M = largestmomentfromfirstorderanalysis(elasticmomentswithout
redistribution)andignoringeffectofimperfections NEd= designvalueofaxialforce ei = eccentricityduetoimperfections=yil0/2
Forcolumnsinbracedsystemsei=l0/400(i.e.yi=l/200formostbracedcolumns).Thedesigneccentricityshouldbeatleast(h/30)butnotlessthan20mm.
where y = inclinationusedtorepresentimperfections l0 = effectivelengthofcolumn h = depthofthesectionintherelevantdirection
Slender columns (nominal curvature method)Thismethodisprimarilysuitableforisolatedmemberswithconstantnormalforceandadefinedeffectivelength l0.Themethodgivesanominalsecondordermomentbasedonadeflection,whichinturnisbasedontheeffectivelengthandanestimatedmaximumcurvature. Other methodsareavailableinBSEN1992-1-1.
Thedesignmomentis:MEd=M0Ed+M2
where
BS EN 1992-1-1 5.8.3.1(1) & NA
BS EN 1992-1-15.8.8.1(1)
BS EN 1992-1-1 5.8.3.1(1)
BS EN 1992-1-1 5.2.7
BS EN 1992-1-1 6.1(4)
BS EN 1992-1-1 5.8.3.2(3)
BS EN 1992-1-15.8.8.2(1)
5.6.2
BS EN 1992-1-1 5.8.4(4)
35
Structuralanalysis
M0Ed = firstordermoment,includingtheeffectofimperfections(andmaybetakenasM0E) M2 = nominalsecondordermoment
ThemaximumvalueofMEdisgivenbythedistributionsofM0EdandM2;thelattermaybetakenasparabolicorsinusoidalovertheeffectivelength.
Forbracedstructures (seeFigure5.8):
MEd=MAX{M0e+M2;M02;M01+0.5M2}
Forunbracedstructures:
MEd=M02+M2
Formomentswithoutloadsappliedbetweentheirends,differingfirstorderendmomentsM01
andM02(seeabove)maybereplacedbyanequivalentfirstorderendmomentM0e:M0e=0.6M02+0.4M01≥0.4M02
ThenominalsecondordermomentM2is
M2=NEde2
where NEd = designvalueofaxialforce e2 = deflection = (1/r)lo
2/c 1/r = curvature=KrKh(fyd/(Es0.45d))
Kr = (nu–n)/(nu–nbal)≤1.0
Note:Krmaybederivedfromcolumncharts.
nu = 1+w w = mechanicalreinforcementratio =(As /Ac)( fyd/fcd)asinSection5.6.1above n = NEd/Ac fcdasdefinedinSection5.6.1above nbal = valueofnatmaximummomentofresistanceandmaybetakenas0.4 Kh =1+bhef≥1.0
b = 0.35+(fck/200)–(l/150)
l = slendernessratiol0 /i
PD 6687-12.11
BS EN 1992-1-15.8.8.2(2)
BS EN 1992-1-15.8.8.2(3)
BS EN 1992-1-15.8.8.2(4)
BS EN 1992-1-1 5.8.8.3
Figure 5.8Moments in
braced columns
+ =
a) First order moments for non-slender columns
b) Additional second order moments for slender columns
c) Total moment diagram for slender columns
M2=NEde2
M02
M02M e1NEd
M0eM0e+M2
M01 0.5M2 M01+0.5M2
36
i = radiusofgyrationoftheuncrackedconcretesection hef = effectivecreepcoefficientasdefinedinSection5.6.1 l0 = effectivelengthofcolumn Es = 200GPa c = factordependingonthecurvaturedistribution(seebelow)
Forconstantcrosssection,c=10(≈p2)isnormallyused.Ifthefirstordermomentisconstant,alowervalueshouldbeconsidered(8isalowerlimit,correspondingtoconstanttotalmoment).
Biaxial bending
Separatedesignineachprincipaldirection,disregardingbiaxialbending,maybeundertakenasafirststep.Nofurthercheckisnecessaryif:
0.5 ≤ ly/lz≤2.0and,forrectangularsections,and0.2 ≥ (ey/heq)/(ez/beq)≥5.0
where
ly,lz = slendernessratiosl0/iwithrespecttothey-andz-axes
ey = MEdy/NEd
heq = 3.46iz (=hforrectangularsections)
ez = MEdz/NEd
beq = 3.46iy (=bforrectangularsections)
where NEd = designvalueofaxialforce MEdy,MEdz= designmomentintherespectivedirection.(Momentsdueto
imperfectionsneedbeincludedonlyinthedirectionwheretheyhavethemostunfavourableeffect.)
Note:forsquarecolumns(ey/heq)/(ez/beq)=MEdy/MEdz
Ifthisconditionisnotsatisfied,andintheabsenceofanaccuratecross-sectiondesignforbiaxialbending,thefollowingsimplifiedcriterionmaybeused:
(MEdz/MRdz)a+(MEdy/MRdy)a≤1.0
where MRdy,MRdz = designmomentaroundtherespectiveaxisincludingsecondordermoment inthedirectionwhereitwillgivethemostunfavourableeffect. a = anexponent:forcircularorellipticalsections,a=2.0,forrectangular
sections,interpolatebetween = 1.0forNEd/NRd=0.1 = 1.5forNEd/NRd=0.7 = 2.0forNEd/NRd=1.0
Corbels
Definition
Corbelsareshortcantileversprojectingfromcolumnsorwallswiththeratioofshearspan(i.e.thedistancebetweenthefaceoftheappliedloadandthefaceofthesupport)tothedepthofthecorbelintherange0.5to2.0.
5.6.3
5.7
5.7.1
BS EN 1992-1-15.8.9(2)
BS EN 1992-1-15.8.9(3)
BS EN 1992-1-15.8.9(2)
BS EN 1992-1-15.8.9(4)
BS EN 1992-1-1 3.2.7(4)
BS EN 1992-1-1 5.8.8.2(4)
37
StructuralanalysisStructuralanalysis
Analysis
Corbels(ac<z0)maybedesignedusingstrutandtiemodels(seeFigure5.9)orasshortbeams
designedforbendingandshear.
Theinclinationofthestrutislimitedby1.0≤tany≤2.5.
Ifac≤0.5hcclosedhorizontalorinclinedlinkswithAs,lnk≥0.5As,mainshouldbeprovidedinadditiontothemaintensionreinforcement(seeFigure5.10a).
Ifac>0.5hcandFEd>VRd,c(seeSection7.2.1)closedverticallinkswithAs,lnk≥0.5FEd/fydshouldbeprovidedinadditiontothemaintensionreinforcement(seeFigure5.10b).
Themaintensionreinforcementshouldbeanchoredatbothends.Itshouldbeanchoredinthesupportingelementonthefarfaceandtheanchoragelengthshouldbemeasuredfromthe location of the vertical reinforcement in the near face.The reinforcement should beanchoredinthecorbelandtheanchoragelengthshouldbemeasuredfromtheinnerfaceoftheloadingplate.
If there are special requirements for crack limitation, inclined stirrups at the re-entrantopeningcanbeeffective.
ThecheckofthecompressionstrutcaneffectivelybemadebylimitingtheshearstresssuchthatFEd≤0.5bwdv'fcd
where v' = 1–(fck/250)
fcd = accfck/gC
acc= 0.85
FEd
Ftd
FEd
aH
HEd
z0hc
d
y
sRd,max
ac
Fwd
Key
Fwd = designvalueofforce
instirrup
= tie
= compressionstrut
Figure 5.9Corbel strut-and-tie model
PD 6687 B3
BS EN 1992-1-16.5.2(2)
PD 6687fig. B4
5.7.2
38
5.8
As,mainAnchorage devices
or loops
Links
a) Reinforcement for ac ≤ 0.5hc b) Reinforcement for ac > 0.5hc
As,lnk ≥ k1As,main
SAs,lnk ≥ As,main
Figure 5.10Corbel detailing
Lateral instability of slender beams
Lateralinstabilityofslenderbeamsshallbetakenintoaccountwherenecessary,e.g.forprecastbeamsduringtransportanderection,forbeamswithoutsufficientlateralbracinginthefinishedstructureetc.Geometricimperfectionsshallbetakenintoaccount.Alateraldeflectionofl/300should be assumed as a geometric imperfection in the verification of beams in unbracedconditions, with l = total length of beam. In finished structures, bracing from connectedmembersmaybetakenintoaccount
Second order effects in connection with lateral instability may be ignored if the followingconditionsarefulfilled:
persistentsituations:l0t/b≤50/(h/b)1/3andh/b≤2.5transientsituations:l0t/b≤70/(h/b)1/3andh/b≤3.5
where l0t= distancebetweentorsionalrestraints h = totaldepthofbeamincentralpartofl0t b = widthofcompressionflange
Torsionassociatedwithlateralinstabilityshouldbetakenintoaccountinthedesignofsupportingstructures.
PD 6687fig. B5
BS EN 1992-1-15.9
39
Bendingandaxialforce
Bending and axial force
Assumptions
Indeterminingtheresistanceofsections,thefollowingassumptionsaremade.
■ Planesectionsremainplane.■ Straininthebondedreinforcement,whetherintensionorcompression,isthesameasthat
inthesurroundingconcrete.■ Tensilestrengthoftheconcreteisignored.■ RectangularstressdistributioninthesectionisasshowninFigure6.1.Otherstress–strain
relationshipsaregiveninBSEN1992-1-1Cl.3.1.7.■ StressesinreinforcementarederivedfromFigure6.2.Theinclinedbranchofthedesignline
maybeusedwhenstrainlimitsarechecked.■ Forsectionsnotfullyincompression,thecompressivestraininconcreteshouldbelimited
toecu2(seeFigure6.3).■ Forsectionsinpureaxialcompression,thecompressivestraininconcreteshouldbelimited
toec2(seeFigure6.3).■ Forsituationsintermediatebetweenthesetwoconditions,thestrainprofileisdefinedby
assumingthatthestrainisec2athalfthedepthofthesection(seeFigure6.3).
ExpressionsderivedfromFigures6.1to6.3areprovidedinSection17.
Table 6.1
Values for n and l when fck > 50
fck ecu3a nb lc
55 0.00313 0.98 0.79
60 0.00288 0.95 0.78
70 0.00266 0.90 0.75
Key
a ecu3(%)=2.6+35[(90–fck)/100]4
b n =1–(fck–50)/200
c l =0.8–(fck–50)/400
BS EN 1992-1-1 fig. 6.1
BS EN 1992-1-1 3.1.7(3), fig. 3.5
BS EN 1992-1-16.1(2)
BS EN 1992-1-1 fig. 3.5
6
6.1
ecu3
fyd
Fs
Fc
nfcd
Ac x l x
d
As
es
z
Forfck ≤ 50MPa,ecu3=0.0035,n =1andl=0.8.ForotherconcreteclassesseeTable6.1
x = neutralaxisdepth Fc(Fs) = forceinconcrete(steel)
ecu3 = ultimatecompressivestraininconcrete d = effectivedepth
es = tensilestraininreinforcement z = leverarm
Figure 6.1Rectangular stress distribution
40
euk
Idealised
Design
Strain, e
Stre
ss, s
eud
fyk
kfyk
fyd=fyk/gS
kfyk/gS
kfyk
fyd/Es
BS EN 1992-1-1fig. 3.8
Where
k = (ft/fy)k(SeeTable3.3)
fyk = characteristicyieldstrengthofreinforcement
fyd = designyieldstrengthofreinforcement
ft = tensilestrengthofreinforcement
gS = partialfactorforreinforcingsteel= 1.15eud= designstrainlimitforreinforcing
steel= 0.9eukeuk = characteristicstrainofreinforcementat
maximumforce(seeTable3.3)
Figure 6.2Idealised and design stress–strain diagrams for reinforcing steel (for tension and compression)
ep(0)
eudec2 ecu2
(ecu3)(ec3)
es,ep
Dep
ec
hd
ey
As2
Ap
As1
0
a) Section b) Strain
(1–ec2/ecu2)hor(1–ec3/ecu3)h
Concretecompressionstrainlimit
ConcretepurecompressionstrainlimitReinforcingsteel
tensionstrainlimit
Where
As1 = areaofreinforcingsteelinlayer1
Ap = areaofprestressingsteel
d = effectivedepth
h = overalldepthofsection
ec = compressivestraininconcrete
es = straininreinforcingsteel
ep(0) = initialstraininprestressingsteel
Dep = changeinstraininprestressingsteel
eud = designstrainlimitforreinforcingsteelintension
ec3 = compressivestrainlimitinconcreteforconcreteinpureaxialcompressionassumingbilinearstress–strainrelationship(seeFigure3.4ofBSEN1992-1-1).
ec3(‰) = 1.75forfck≤50MPa
ec3(‰) = 1.75+0.55[(fck–50)/40]forfck>50MPa
ecu2 = (=ecu3)compressivestrainlimitinconcretenotfullyinpureaxialcompression
ecu3(‰)=3.5forfck≤50MPa.
ecu3(‰) = 2.6+0.35[(90–fck)/100]4forfck>50MPa
ey = reinforcementyieldstrain
Figure 6.3Possible strain distributions in the ultimate limit state
BS EN 1992-1-1fig. 6.1
41
Shear
Shear
General
Definitions
Fortheverificationoftheshearresistancethefollowingsymbolsaredefined:VRd,c = designshearresistanceofamemberwithoutshearreinforcementVRd,s = designvalueoftheshearforcethatcanbesustainedbytheyieldingshear
reinforcementVRd,max = designvalueofthemaximumshearforcethatcanbesustainedbythemember,
limitedbycrushingofthecompressionstruts
Theseresisttheappliedshearforce,VEd.
Requirements for shear reinforcement
If VEd ≤ VRd,c, no calculated shear reinforcement is necessary. However, minimum shearreinforcementshouldstillbeprovided(seeSection15.2.6)exceptin:
■ Slabs,whereactionscanberedistributedtransversely.Membersofminorimportance,whichdonotcontributesignificantlytotheoverall■■
resistanceandstabilityofthestructure(e.g.lintelswithaspanoflessthan2m).
If VEd > VRd,c shear reinforcement is required such that VRd,s > VEd.The resistance of theconcretetoactasastrutshouldalsobechecked.
Inmemberssubjectpredominantlytouniformlydistributedloading,thefollowingapply:
Shearatthesupportshouldnotexceed■■ VRd,max.Requiredshearreinforcementshouldbecalculatedatadistance■■ dfromthefaceofthesupportandcontinuedtothesupport.
The longitudinaltensionreinforcementshouldbeabletoresisttheadditionaltensile forcecausedbyshear(seeSection15.2.2).
TheUKNAlimitsshearstrengthofconcretehigherthanC50/60tothatofC50/60.
Shear and transverse bending
Duetothepresenceofcompressivestressfieldsarisingfromshearandbending,theinteractionbetweenlongitudinalshearandtransversebendinginthewebsofboxgirdersectionsshouldbeconsideredinthedesign.WhenVEd/VRd,max<0.2orMEd/MRd,max<0.1,thisinteractioncanbedisregarded(whereVRd,maxandMRd,maxrepresentrespectivelythemaximumwebcapacityforlongitudinalshearandtransversebending).
FurtherinformationontheinteractionbetweenshearandtransversebendingmaybefoundinAnnexMMofBSEN1992-2.
Resistance of members not requiring shear reinforcement
General situation
Thedesignvaluefortheshearresistanceisgivenby:
VRd,c= [(0.18/gC)k(100rlfck)1/3+0.15scp]bwd
≥ ( 0.035k1.5fck0.5 +0.15scp)bwd
BS EN 1992-1-1 6.2.1(1)
BS EN 1992-1-1 6.2.1(3)
BS EN 1992-1-1 6.2.1(4)
BS EN 1992-1-1 6.2.1(5)
BS EN 1992-1-1 6.2.1(8)
BS EN 1992-1-1 6.2.1(7)
BS EN 1992-2 3.1.2(2) & NA
BS EN 1992-26.2.106 (101)
BS EN 1992-26.2.2(101) & NA
7
7.1
7.1.1
7.1.2
7.1.3
7.2
7.2.1
42
where k = 1+(200/d)0.5≤2.0(dinmm;seeTable7.1) gC= 0.15 rl = Asl/(bwd)≤0.02
where Asl = areaofthetensilereinforcementextendingatleastlbd+dbeyondthesection
considered(seeFigure7.1);theareaofbondedprestressingsteelmaybeincludedinthecalculationofAsl.Inthiscaseaweightedmeanvalueofdmaybeused.
lbd = designanchoragelength bw = smallestwidthofthecross-sectioninthetensilearea scp= NEd/Ac<0.2fcd(MPa)
where NEd = axialforceinthecross-sectionduetoloadingorprestressinginnewtons
(NEd>0forcompression).TheinfluenceofimposeddeformationsonNEdmaybeignored.
AC = areaofconcretecross-section(mm2)
Table 7.1
VRd,c ' shear resistance without shear reinforcement where scp = 0 (MPa)
rl = As/(bd) Effective depth d (mm)
≤200 225 250 275 300 350 400 450 500 600 750
0.25% 0.54 0.52 0.50 0.48 0.47 0.45 0.43 0.41 0.40 0.38 0.36
0.50% 0.59 0.57 0.56 0.55 0.54 0.52 0.51 0.49 0.48 0.47 0.45
0.75% 0.68 0.66 0.64 0.63 0.62 0.59 0.58 0.56 0.55 0.53 0.51
1.00% 0.75 0.72 0.71 0.69 0.68 0.65 0.64 0.62 0.61 0.59 0.57
1.25% 0.80 0.78 0.76 0.74 0.73 0.71 0.69 0.67 0.66 0.63 0.61
1.50% 0.85 0.83 0.81 0.79 0.78 0.75 0.73 0.71 0.70 0.67 0.65
1.75% 0.90 0.87 0.85 0.83 0.82 0.79 0.77 0.75 0.73 0.71 0.68
≥ 2.00% 0.94 0.91 0.89 0.87 0.85 0.82 0.80 0.78 0.77 0.74 0.71
k 2.000 1.943 1.894 1.853 1.816 1.756 1.707 1.667 1.632 1.577 1.516
Notes
1 TablederivedfromBSEN1992-1-1andtheUKNationalAnnex.
2 Tablecreatedforfck=30MPaassumingverticallinks.
3 Forrl≥0.4%andfck = 25MPa,applyfactorof0.94 fck = 45MPa,applyfactorof1.14 fck = 35MPa,applyfactorof1.05 fck ≥ 50MPa,applyfactorof1.19 fck = 40MPa,applyfactorof1.10
Uncracked regions in prestressed membersIn prestressed single-span members without shear reinforcement, the shear resistance of theregionscrackedinbendingmaybecalculatedusingtheExpressioninSection7.2.1.Inregionsuncracked in bending (where the flexural tensile stress is smaller than fctk,0.05/gC) the shearresistanceshouldbelimitedbythetensilestrengthoftheconcrete.Intheseregionstheshearresistanceisgivenby:
VRd,c=(Ibw/S)(fctd2+alscpfctd)0.5
where I = secondmomentofarea
bw = widthofthecross-sectionatthecentroidalaxis,allowingforthepresenceofducts(seebelow)
BS EN 1992-1-1 6.2.2(2)
7.2.2
43
Shear
S = firstmomentofareaaboveandaboutthecentroidalaxis
al = lx/lpt2≤1.0forpretensionedtendons
= 1.0forothertypesofprestressing
lx = distanceofsectionconsideredfromthestartingpointofthetransmissionlength
lpt2= upperboundvalueofthetransmissionlengthoftheprestressing(Seesection14.6)
scp= concretecompressivestressatthecentroidalaxisduetoaxialloadingand/orprestressing(scp=NEd /AcinMPa,NEd>0incompression)
Alternatively,wherethereisnoaxialforce,includingprestressingVRd,c=bwdvRd,cwithvRd,cavailablefromTable7.1
InmostpracticalcasesifvEd<vRd,cshearreinforcementwillnotberequired
where
vEd = shearstressforsectionswithoutshearreinforcement=VEd/bwd.
vRd,c maybeinterpolatedfromTable7.1.
Short span shear enhancement
TheapproachinBSEN1992-1-1ofapplyingareductionfactortotheloadisnotsuitableforcaseswithmultiple,indirectordistributedloads.Therefore,intheNAtoBSEN1992-2,theexpressionforCRd,chasbeenmodifiedfromtherecommendedvaluesothattheeffectsofshearenhancementaretakenintoaccountthroughincreasingtheshearresistanceofmembersneartosupports.SeeFigure7.2.
Formemberswithactionsappliedatadistanceavwhere0.5d≤av≤2d:
kgC(100r1 fck)b + 0.15scpVRd,c =
0.18av
2d[ ] bw d
providedthattheshearforce,VEd,isnotmultipliedbyb(BSEN1992-1-1,Cl.6.2.2(6))andthelongitudinalreinforcementisfullyanchoredatthesupport.
Figure 7.1Definition of Asl
a) End support
b) Internal support
Sectionconsidered Section
considered
Sectionconsidered
45º
45º
Asl Asl
Asl
Ibd Ibd
Ibd
VEd VEd
VEd
d
d
45º
BS EN 1992-2 fig. 6.3
BS EN 1992-2 NA 6.2.2(101)
PD 6687-2 7.2.2
7.2.3
44
Figure 7.2Loads near supports b) Corbel
av
a) Beam with direct support
av
d
d
Resistance of members requiring shear reinforcement
Basis
ThedesignofmemberswithshearreinforcementisbasedonthetrussmodelshowninFigure7.3. AsimplifiedversionofthisdiagramisshowninFigure7.4.
b) Web thickness bw
bw bw
a) Truss model
Ftd
d
TensilechordShearreinforcement
CompressionchordStruts
Fcd
s
VM
N
V
V(coty–cota)
ya
z=
0.9daz
az
Figure 7.3Truss model and notation for shear reinforced members
Figure 7.4Variable strut angle, y
Concretestrutincompression
Longitudinalreinforcementintension
Verticalshearreinforcement
y
BS EN 1992-2 fig. 6.5
BS EN 1992-1-1 6.2.3
7.3
7.3.1
BS EN 1992-1-1 fig. 6.4
45
Shear
Shear resistance check
TheresistanceoftheconcretesectiontoactasastrutVRd,maxshouldbecheckedtoensurethatitequalsorexceedsthedesignshearforce,VEdi.e.ensurethat:
VRd,max = acwbwzv1fcd(coty+tany)≥VEdwithverticallinks = acwbwzv1fcd(coty+cota)/(1+cot2y)≥VEdwithinclinedlinkswhere z = leverarm(SeeSection7.3.3)
v1 = 0.6[1–(fck/250)](1–0.5cosa) fcd = 1.0 fck/ 1.5 y = angleofinclinationofthestrut,suchthatcotyliesbetween1.0and2.5. a = angleofinclinationofthelinkstothelongitudinalaxisForverticallinkscota=0. acw = coefficienttakingaccountofthestateofthestressinthecompressionchord(see
Table7.2) = 1 fornon-prestressedstructures
= (1+scp/fcd)for0<scp≤0.25fcd
= 1.25for0.25fcd<scp≤0.5fcd
= 2.5(1–scp/fcd)for0.5fcd<scp<1.0fcd
where scp=meancompressivestress,measuredpositive,intheconcreteduetothedesign
axialforce.
scpshouldbeobtainedbyaveragingitovertheconcretesectiontakingaccountofthereinforcement.Thevalueofscpneednotbecalculatedatadistancelessthan0.5dcotyfromtheedgeofthesupport.
The values ofv1 andacw should not give rise to a value of VRd,max greater than 200bw2 at
sectionsmorethanadistancedfromtheedgeofasupport.Forthispurpose,thevalueofbwdoesnotneedtobereducedforducts.
Table 7.2Values for acw
fck fcd Mean compressive stress, scp
0 0.5 1 2 3 4 5 10 20 30
20 13.3 1 1.04 1.08 1.15 1.23 1.25 1.25 0.63 — —
25 16.7 1 1.03 1.06 1.12 1.18 1.24 1.25 1.00 — —
30 20.0 1 1.03 1.05 1.10 1.15 1.20 1.25 1.25 — —
35 23.3 1 1.02 1.04 1.09 1.13 1.17 1.21 1.25 0.36 —
40 26.7 1 1.02 1.04 1.08 1.11 1.15 1.19 1.25 0.63 —
45 30.0 1 1.02 1.03 1.07 1.10 1.13 1.17 1.25 0.83 —
50 33.3 1 1.02 1.03 1.06 1.09 1.12 1.15 1.25 1.00 0.25
60 40.0 1 1.01 1.03 1.05 1.08 1.10 1.13 1.25 1.25 0.63
70 46.7 1 1.01 1.02 1.04 1.06 1.09 1.11 1.21 1.25 0.89
In the case of straight tendons, a high level of prestress (scp/fcd > 0.5) and thin webs, if thetensionandthecompressionchordsareabletocarrythewholeprestressingforceandblocksareprovidedattheextremityofbeamstodispersetheprestressingforce(seeFigure7.5),itmaybeassumedthattheprestressingforceisdistributedbetweenthechords.Inthesecircumstances,thecompressionfieldduetoshearonlyshouldbeconsideredintheweb(acw=1).
Pd
Pd,t
Pd,c
Pd = Pd,c + Pd,t
Figure 7.5Dispersion of prestressing by end blocks within the chords
BS EN 1992-2 6.2.3(103) & NA
BS EN 1992-2 6.2.3(103) & NA
BS EN 1992-2 fig. 6.101
7.3.2
BS EN 1992-1-1 Exp. (6.9) Exp. (6.14) & NA
46
Themaximumeffectivecross-sectionalareaoftheshearreinforcementAsw,maxforcoty=1isgivenby:
aacwv1 fcdAsw,max fywd
bw s≤
Lever arm, z
Intheshearanalysisofreinforcedconcrete,theapproximatevaluez=0.9dmaynormallybeused.Thisisnotappropriatewhen:
Thereisanaxialforceorprestress,or■■
Thewidthatthecentroidisgreaterthantheminimumcross-sectionwidthin■■
compression,orThecross-sectionhasatensionflangebutnocompressionflange■■
Insuchcasestheleverarmshouldbedeterminedbasedonananalysisofthesection.
Shear reinforcement required, Asw/s
The cross-sectional area of the shear reinforcement required is calculated using the shearresistance:
VRd,s=(Asw/s) z fywd(coty+cota)sina≤VRd,max
where Asw = cross-sectionalareaoftheshearreinforcement.(ForAsw,minseeSection15.2.6) s = spacingofthestirrups z = leverarm(SeeSection7.3.3) fywd= fywk/gS=designyieldstrengthoftheshearreinforcement
a = angleofthelinkstothelongitudinalaxis
Forverticallinks,cota=0andsina=1.0,and:
Asw/s≥VEd/ (z fywdcoty)
Webs containing metal ducts
Wherethewebcontainsgroutedmetalductswithadiameterf>bw/8theshearresistancevRd,maxshouldbecalculatedonthebasisofanominalwebthicknessgivenby:
bw,nom=bw–0.5SfwherefistheouterdiameteroftheductandSfisdeterminedforthemostunfavourablelevel.
Forgroutedmetalductswithf≤bw/8,bw,nom=bw
Fornon-groutedducts,groutedplasticductsandunbondedtendonsthenominalwebthicknessis:
bw,nom=bw–1.2Sf
Thevalue1.2isintroducedtotakeaccountofsplittingoftheconcretestrutsduetotransversetension.Ifadequatetransversereinforcementisprovidedthisvaluemaybereducedto1.0.
Additional tensile forces
Theadditionaltensile force,D Ftd, inthe longitudinal reinforcementduetoshearVEdmaybecalculatedfrom:
D Ftd=0.5VEd(coty–cota)MEd/z+D FtdshouldbetakenasnotgreaterthanMEd,max/z
BS EN 1992-1-1 Exp. (6.15)
BS EN 1992-1-1 Exp. (6.13)
PD 6687-2 7.2.4.1
BS EN 1992-1-16.2.3(1)
BS EN 1992-1-1 Exp. (6.8)
BS EN 1992-1-1 6.2.3(6)
BS EN 1992-1-1 Exp. (6.16)
BS EN 1992-1-1Exp. (6.17)
BS EN 1992-1-1Exp. (6.18)
7.3.3
7.3.4
7.3.5
7.3.6
47
Shear
where MEd,max=maximummomentalongthebeam
Thisadditionaltensileforcegivesrisetothe‘shift’ruleforthecurtailmentofreinforcement(seeSection15.2).
In the case of bonded prestressing, located within the tensile chord, the resisting effect ofprestressingmaybetakenintoaccountforcarryingthetotallongitudinaltensileforce.Inthecase of inclined bonded prestressing tendons in combination with other longitudinalreinforcement/tendonstheshearstrengthmaybeevaluated,byasimplification,superimposingtwodifferenttrussmodelswithdifferentgeometry(Figure7.6);aweightedmeanvaluebetweeny1andy2maybeusedforconcretestressfieldverificationwithExpression(6.9).
y2y1
Figure 7.6Superimposed resisting model for shear
Members with actions applied near bottom of section
Whereloadisappliednearthebottomofasection,sufficientshearreinforcementtocarrytheload to the top of the section should be provided in addition to any shear reinforcementrequiredtoresistshear.
Shear between web and flanges of T-sections
Thelongitudinalshearstress,vEd,atthejunctionbetweenonesideofaflangeandthewebisdeterminedbythechangeofthenormal(longitudinal)forceinthepartoftheflangeconsidered,accordingto:
vEd=DFd/(hfDx)
where hf = thicknessofflangeatthejunctions Dx = lengthunderconsideration,seeFigure7.7 DFd = changeofthenormalforceintheflangeoverthelengthDx
A
A
Fd
Fd
Sf
beff
Asf
hf
Fd + DFd
Fd + DFd
Dx
bw
yf
Longitudinal baranchored beyondthis projected point
Compressive struts
Figure 7.7Notations for the connection between flange and web
BS EN 1992-2 6.2.3(107)
BS EN 1992-2 fig. 6.102N
BS EN 1992-1-1 6.2.1(9)
BS EN 1992-26.2.4(103)
BS EN 1992-1-1fig. 6.7
7.3.7
7.3.8
48
ThemaximumvaluethatmaybeassumedforDxishalfthedistancebetweenthesectionwherethemomentis0andthesectionwherethemomentismaximum.WherepointloadsareappliedthelengthDxshouldnotexceedthedistancebetweenpointloads.
Alternatively,consideringalengthDxofthebeam,thesheartransmittedfromthewebtotheflangeisvEdDx/zandisdividedintothreeparts:oneremainingwithinthewebbreadthandtheothertwogoingouttotheflangeoutstands.Itshouldbegenerallyassumedthattheproportionof the force remaining within the web is the fraction bw/beff of the total force. A greaterproportion may be assumed if the full effective flange breadth is not required to resist thebendingmoment.InthiscaseacheckforcracksopeningatSLSmaybenecessary.
Therateofchangeoftheflangeforcescanbeunderestimatediftheeffectsofwebshearontheflangeforcesarenotincluded,particularlyforcompressionflanges.Thechordforcesasdeterminedforthedesignofthewebreinforcementshouldthereforebeused.
Forcompressionflanges,Fdmaybecalculatedasfollows:
Fd=(beff–bw)Fcd/(2beff)whenhf>xcFd=(beff–bw)fcdhf/2 whenhf≤xc
where xc = depthofthecompressionzone Fcd = totalforceinthecompressionchordofthesheartrussintheweb
Fortensionflanges,Fdmaybecalculatedbydeterminingtheproportionofthetotaltensionchordforce,Ftd,carriedineachsideoftheflange.
ThetransversereinforcementperunitlengthAsf /sfmaybedeterminedasfollows:
(Asf fyd /sf)≥vEdhf/cotyf
Topreventcrushingofthecompressionstrutsintheflange,thefollowingconditionshouldbesatisfied:
VEd≤ 0.6(1–fck/250) fcdsinyfcosyf
where
fcd= 1.0 fck/ 1.5
Thepermittedrangeofthevaluesforcotyfare:
1.0 ≤cotyf≤ 2.0 forcompressionflanges(45°≥yf≥26.5°)
1.0 ≤cotyf≤1.25fortensionflanges(45°≥yf≥38.6°)
IfvEdislessthanorequalto 0.4 fctdnoextrareinforcementabovethatforflexureisrequired.
Longitudinaltensionreinforcementintheflangeshouldbeanchoredbeyondthestrutrequiredto transmit the force back to the web at the section where this reinforcement is required(SeeSection(A–A)ofFigure7.7).
Interface shear between concretes placed at different times
Whencompositeactionisassumedbetweentwolayersofconcretecastatdifferenttimes,itisnecessarytopreventslipbetweenthetwolayers.Thiswillresultinshearstressattheinterface,whichshouldbeverified.Theforceattheinterfaceistheflangeforceinthenewconcretecausedbythebendingmomentonthecompositesection.
The shear stress at the interface between concrete cast at different times should satisfy thefollowing.
vEdi≤vRdi
PD 6687-2, 7.2.5
BS EN 1992-1-1 6.2.4(4)
BS EN 1992-1-1 6.2.4(6)
BS EN 1992-1-16.2.5
7.3.9
49
Shear
where
vEdi=designvalueoftheshearstressintheinterfaceandisgivenby:
vEdi=b VEd /(zbi)
where VEd= transverseshearforce z = leverarmofthecompositesection bi = widthoftheinterface(seeFigure7.8) b = ratioofthelongitudinalforceinthenewconcreteandthetotallongitudinalforce
eitherinthecompressionortensionzone,bothcalculatedforthesectionconsidered
vRdi=cfctd+μsn+rfyd(μsina +cosa)≤0.5 0.6(1–fck/250) fcd
where
thevaluesofcandμdependontheinterfacesurfaceandareshowninTable7.3 fctd= fctk,0.05/ 1.5
fcd = 1.0 fck/ 1.5 sn= stressnormaltotheinterfacenottobetakengreaterthan0.6fcd
r = As/Ai
As = areaofreinforcementcrossingtheinterfaceincludingordinaryshearreinforcement(ifany),withadequateanchorageatbothsidesoftheinterface
Ai = areaofthejoint a =angleofreinforcementcrossingtheinterface(45°≤a ≤90°)
bi
bi
a) Double-T unit with topping b) I-beam with topping
Figure 7.8Examples of interfaces for shear
Table 7.3Values of m and c for various interfaces
Classification of interface surfaces Friction coefficient, m Shear coefficient, c
Very smooth: surface cast against steel, plastic or smooth wooden moulds
0.5 0.10
Smooth: slipformed or extruded surface or face untreated after vibration
0.6 0.20
Rough: a surface with at least 3 mm roughness at 40 mm spacing
0.7 0.40
Whereasteppeddistributionoftransversereinforcementisused,thetotalresistancewithinanybandofreinforcementshouldbenotlessthanthetotallongitudinalshearinthesamelength and the longitudinal shear stress evaluated at any point should not exceed theresistanceevaluatedlocallybymorethan10%.
BS EN 1992-1-1 fig. 6.8
BS EN 1992-1-16.2.5(2)
PD 6687-2 7.2.6
50
8
8.1
8.1.1
8.1.2
8.2
8.2.1
Punching shear
General
Basis of design
Punching shear is a local shear failure around concentrated loads on slabs and the mostcommonsituationswherethepunchingshearrulesarerelevantinbridgeapplicationsareinthedesignofpilecaps,padfootings,anddeckslabswhicharesubjectedtowheelloadsandaroundsupportsinslabssupportedondiscretebearingsorcolumns.Theresultingstressesareverifiedalongdefinedcontrolperimetersaroundtheloadedarea.Theshearforceactsoveranareaudeff,whereu isthelengthoftheperimeteranddeff istheeffectivedepthoftheslabtakenastheaverageoftheeffectivedepthsintwoorthogonaldirections.
Design procedure
Atthecolumnperimeter,ortheperimeterofthe loadedarea,themaximumpunchingshearstressshouldnotbeexceeded,vEd≤vRd,max.
Punchingshearreinforcementisnotnecessaryif
vEd≤vRd,c
WherevEdexceedsvRd,cforthecontrolsectionconsidered,punchingshearreinforcementshouldbeprovidedaccordingtoSection8.5
where
vEd = designvalueoftheappliedshearstress(seeSections8.2and8.3) vRd,max= designvalueofthemaximumpunchingshearresistance(seeSection8.6)along
thecontrolsectionconsidered vRd,c = designvalueofpunchingshearresistanceofaslabwithout punchingshear
reinforcement,alongthecontrolsectionconsidered(seeSection8.4) vRd,cs = designvalueofpunchingshearresistanceofaslabwith punchingshear
reinforcement,alongthecontrolsectionconsidered(seeSection8.5)
Applied shear stress
General
Where the support reaction is eccentric with regard to the control perimeter, the maximumshearstressshouldbetakenas:
vEd=b VEd /(uid)
where d = meaneffectivedepth
= (dy+dz)/2
ui = lengthofthecontrolperimeterunderconsideration(seeSection8.3)
VEd = designvalueofappliedshearforce
b = factordealingwitheccentricity
dy = effectivedepthiny-direction
dz = effectivedepthinz-direction
BS EN 1992-1-16.4.3(1)
BS EN 1992-1-16.4.3(3)
BS EN 1992-1-16.4.3(2)
BS EN 1992-1-16.4.1
51
Punchingshear
8.2.2
8.2.3
Values of b (conservative values from diagram)
Forbracedstructures,whereadjacentspansdonotdifferbymorethan25%,thevaluesofbshowninFigure8.1maybeused.
Cornercolumn
Edgecolumn Internalcolumn
b =1.5
b =1.4 b =1.15
Figure 8.1Recommended values for b
Values of b (using calculation method)
As an alternative to Section 8.2.2, the values of b can be obtained using the followingmethods.
Internal columnsForinternalrectangularcolumnswithloadingeccentricto■■ oneaxis:
b=1+(kMEd/VEd)(u1/W1)
where k = coefficientdependingontheratioofthecolumndimensionsc1andc2as
showninFigure8.2(seeTable8.1) MEd= designvalueoftheappliedinternalbendingmoment u1 = lengthofthebasiccontrolperimeter(seeFigure8.3) W1 = adistributionofshearasillustratedinFigure8.2andisafunctionofu1 W1 = c1
2/2+c1c2+4c2d+16d2+2pdc1forarectangularcolumn
=ʃui|e|dl forthegeneralcase 0
where
||= theabsolutevalue e = thedistanceofdlfromtheaxisaboutwhichMEdacts dl = alengthincrementoftheperimeter
2d
2d
c1
c2
Figure 8.2Shear distribution due to an unbalanced moment at a slab/ internal column connection
BS EN 1992-1-1 6.4.3(6)
BS EN 1992-1-1 fig. 6.21N & NA
BS EN 1992-1-1 Exp. (6.39)
BS EN 1992-1-1 Exp. (6.40)
BS EN 1992-1-1 fig. 6.19
52
Table 8.1Values for k for rectangular loaded areas
c1/c2 ≤ 0.5 1.0 2.0 ≥ 3.0
k 0.45 0.60 0.70 0.80
Forinternalrectangularcolumnswithloadingeccentricto■■ both axes: b=1+1.8[(ey/bz)2+(ez/by)2]0.5
where eyandez = MEd/VEdalongyandzaxesrespectively byandbz = thedimensionsofthecontrolperimeter(seeFigure8.3)
Forinternalcircularcolumns:■■
b=1+0.6pe/(D+4d)
where D = diameterofthecircularcolumn e = MEd/VEd
u1=basiccontrolperimeter
2d2d
2d
2d
u1
u1u1
by
bz
Figure 8.3Typical basic control perimeters around loaded areas
Edge columns
Foredgecolumns,withloadingeccentricityperpendicularandinteriortotheslabedge,■■
b=u1/u1*
where u1 = basiccontrolperimeter(seeFigure8.4) u1*= reducedcontrolperimeter(seeFigure8.5)
Foredgecolumns,witheccentricitytobothaxesandinteriortotheslabedge■■
b=u1/u1*+keparu1/W1
where k = coefficientdependingontheratioofthecolumndimensionsc1andc2as
showninFigure8.5(seeTable8.2)
epar= eccentricityparalleltotheslabedgeresultingfromamomentaboutanaxisperpendiculartotheslabedge
W1 = c22/4+c1c2+4c1d+8d2+pdc2
where c1andc2areasinFigure8.5
BS EN 1992-1-1 table 6.1
BS EN 1992-1-1 Exp. (6.43)
BS EN 1992-1-1 Exp. (6.42)
BS EN 1992-1-1 fig. 6.13
BS EN 1992-1-1 6.4.3(4)
BS EN 1992-1-1 Exp. (6.44)
53
Punchingshear
2d
u1
u1
u1
2d 2d
2d
2d
2d
u1=basiccontrolperimeter
Figure 8.4Control perimeters for loaded areas at or close to an edge or corner
≤1.5d
≤1.5d
≤1.5d
≤0.5c1
≤0.5c1
≤0.5c2
2d
2d
2d
2d
c1
c1c2
c2
u1*
u1*
a) Edge column b) Corner column
Figure 8.5Equivalent control perimeter u1*
Table 8.2Values for k for rectangular loaded areas at edge of slabs and subject to eccentric loading in both axes
c1/2c2* ≤ 0.5 1.0 2.0 ≥ 3.0
k 0.45 0.60 0.70 0.80
Note
*differsfromTable8.1
Corner columns Forcornercolumnswitheccentricitytowardsinterioroftheslab
b=u1/u1*
where u1 = basiccontrolperimeter(seeFigure8.4) u1*= reducedcontrolperimeter(seeFigure8.5)
BS EN 1992-1-1 fig. 6.15
BS EN 1992-1-1 fig. 6.20
BS EN 1992-1-1 6.4.3(5)
BS EN 1992-1-1 Exp. (6.46)
54
Perimeter columns where eccentricity is exterior to slab
Foredgeandcornercolumns,whereeccentricityisexteriortotheslabtheexpression
b=1+(kMEd/VEd)(u1/W1i
appliesasforinternalcolumnsabove.However,MEd/VEd(=e,eccentricity)ismeasuredfromthecentroidofthecontrolperimeter.
Control perimeters
Basic control perimeter u1 (internal columns)
Thebasiccontrolperimeteru1maybetakentobeatadistanceof2.0dfromthefaceoftheloadedarea,constructedsoastominimiseitslength(seeinFigure8.3).
Openings
Where openings in the slab exist within 6d from the face of the loaded area, part of thecontrolperimeterwillbeineffectiveasindicatedinFigure8.6.
a) Where l1 l2 b) Where l1 > l2
Opening
2d
≤6d
l2
l1≤l2l1>l2
(l1l2)0.5
u1
Ineffective
Figure 8.6Control perimeter near an opening
Perimeter columns
Foredgeorcornercolumns(orloadedareas),thebasiccontrolperimeteru1showninFigure8.4maybeusedforconcentricloading.ThisperimetermustnotbegreaterthantheperimeterobtainedforinternalcolumnsfromusingFigure8.3(seeSection8.3.1).
Whereeccentricityofloadsisinteriortotheslab,thereducedcontrolperimeter,u1*showninFigure8.5shouldbeusedasindicatedinSection8.2.3.
Column heads
Wherecolumnheadsareprovided,distinctionshouldbemadebetweencaseswherelH>2hHandwherelH<2hH
where
lH = projectionofheadfromthecolumn hH = heightofheadbelowsoffitofslab
BS EN 1992-1-1 6.4.3(4)6.4.3(5)
BS EN 1992-1-1 6.4.2
BS EN 1992-1-1 fig. 6.14
BS EN 1992-1-1 6.4.2(5)
BS EN 1992-1-1 6.4.2(9)
8.3
8.3.1
8.3.2
8.3.3
8.3.4
55
Punchingshear
WherelH<2hHpunchingshearneedstobecheckedonlyinthecontrolsectionoutsidethecolumnhead(seeFigure8.7).WherelH>2hHthecriticalsectionsbothwithintheheadandslabshouldbechecked(seeFigure8.8).
LoadedareaAload
Note
y =26.6º,tany=0.5
hH
rcont rcont
hH
d
lH<2.0hH lH<2.0hH
c
Basiccontrolsection
y
y y
y
Figure 8.7Slab with enlarged column head where lH < 2.0 hH
Note
y=26.6º,tany=0.5
lH>2hH lH>2hH
rcont,ext rcont,ext
rcont,ext rcont,ext
LoadedareaAload
Basiccontrolsectionsforcircularcolumns
d d
hHhH
dH dH
c
y
y y
y
Figure 8.8Slab with enlarged column head where lH > 2hH
Punching shear resistance without shear reinforcement
The punching shear resistance of a slab should be assessed for the basic control sectionaccordingtoSection8.3.Thedesignpunchingshearresistancemaybecalculatedasfollows:
Thedesignvaluefortheshearresistanceisgivenby:
vRd,c = (0.18/gC)k(100rlfck)1/3+0.15scp
≥ 0.035k1.5fck0.5 +0.15scp
where k = 1+(200/d)0.5≤2.0(dinmm) gC= 1.5 rl = (rly,rlz)0.5≤0.02
where rly,rlz= reinforcementratiosintheyandzdirectionsrespectively.Thevaluesshould
becalculatedasmeanvalues,takingintoaccountaslabwidthequaltothecolumnwidthplus3deachside
scp = (scy+scz)/2 scy = NEd,y/Acy scz = NEd,z/Acz
BS EN 1992-1-1 fig. 6.17
BS EN 1992-1-1 fig. 6.18
BS EN 1992-1-1 6.4.4
BS EN 1992-1-1 Exp. (6.47) & NA
8.4
56
where NEd,y,NEd,z = longitudinalforcesacrossthefullbayforinternalcolumnsand
thelongitudinalforcesacrossthecontrolsectionforedgecolumns.Theforcemaybefromaloadorprestressingaction
AC = areaofconcretecross-sectionaccordingtothedefinitionofNEd(mm2)
Punching shear resistance with shear reinforcement
WhereshearreinforcementisrequireditshouldbecalculatedinaccordancewiththeExpressionbelow:
vRd,cs=0.75vRd,c+1.5(d/sr)Aswfywd,ef(1/u1d)sina
where Asw = areaofoneperimeterofshearreinforcementaroundthecolumn(mm2)
(forAsw,minseeSection15.4.3)
sr = radialspacingofperimetersofshearreinforcement(mm)
fywd,ef = effectivedesignstrengthofreinforcement(250+0.25d)≤fywd
d = meaneffectivedepthinthetwoorthogonaldirections(mm)
u1 = basiccontrolperimeterat2dfromtheloadedarea(seeFigure8.3)
sina = 1.0forverticalshearreinforcement
a = anglebetweentheshearreinforcementandplaneoftheslab
AssumingverticalreinforcementAsw=(vEd–0.75vRd,c)sru1/(1.5fywd,ef)perperimeter
Punching shear resistance adjacent to columns
Adjacenttothecolumnthepunchingshearresistanceislimitedtoamaximumof:
vEd=bVEd/u0d≤vRd,max
where b = factordealingwitheccentricity(seeSection8.2) VEd = designvalueofappliedshearforce d = meaneffectivedepth u0 = lengthofcolumnperipheryforaninteriorcolumn
=2(c1+c2)forinteriorcolumns = c2+3d≤c2+2c1foredgecolumns = 3d≤c1+c2forcornercolumns where
c1 = columndepth(foredgecolumns,measuredperpendiculartothefreeedge)c2 = columnwidthasillustratedinFigure8.5
vRd,max=0.5vfcd
where v= 0.6[1–(fck/250)]
Control perimeter where shear reinforcement is no longer required, uout
ShearreinforcementisnotrequiredataperimeterwheretheshearstressduetotheeffectiveshearforcedoesnotexceedvRd,c.Theoutermostperimeterofshearreinforcementshouldbeplacedatadistancenotgreaterthan1.5d withintheperimeterwherereinforcementisnolongerrequired.SeeFigures8.9,15.6and15.7.
8.5
8.6
8.7
BS EN 1992-1-1 6.4.5
BS EN 1992-1-1 Exp. (6.52)
BS EN 1992-1-1 6.4.5(3)
BS EN 1992-1-1 6.4.5(4) & NA
57
Punchingshear
Perimeteruout,efPerimeteruout
≤2d
>2d
d
d
1.5d
1.5d
Figure 8.9Control perimeters at internal columns
Distribution of shear reinforcement
TheExpressiongiveninSection8.5assumesaconstantareaofshearreinforcementoneachperimetermovingawayfromtheloadedareaasshowninFigure8.9.Incaseswherethereinforcementareavariesonsuccessiveperimeters,therequiredshearreinforcementmaybedeterminedbycheckingsuccessiveperimeters,uibetweenthebasiccontrolperimeterandtheperimeteruout,toensurethattheshearreinforcementofareaSAswsatisfiesthefollowingexpression:
fywd, ef sin a SAsw
(vEd – 0.75 vRd, c ) ui d=
where SAsw is the total shear reinforcement as shown in Figure 8.10, placed within anarea enclosed between the control perimeter ui chosen and one 2d inside it, except thatshear reinforcement within a distance of 0.3d from the inner perimeter and 0.2d from thecontrolperimetershouldbeignored.FurtherguidanceandbackgroundaregivenbyHendy&Smith[20]
2d
0.2d0.3d
1
Uout
Ui
Notes1 uiisbetweenu1
anduout
2ReinforcementS Aswtoincludeincludeforcheckonperimeterui
Figure 8.10Reinforcement to include in punching shear check
BS EN 1992-1-1 fig. 6.22
PD 6687-2 7.3.2
8.8
PD 6687-2 fig. 4
58
BS EN 1992-1-1 fig. 6.16
8.9 Punching shear resistance of foundation bases
In addition to the verification at the basic control perimeter at 2d from the face of thecolumn, perimeters within the basic perimeter should also be checked for punchingresistance.Incaseswherethedepthofthebasevaries,theeffectivedepthofthebasemaybeassumedtobethatattheperimeteroftheloadedarea.SeeFigure8.11.
Forconcentricloadingthenetappliedforceis
VEd,red=VEd–DVEd
where VEd = appliedshearforce DVEd = netupwardforcewithintheperimeterconsidered,i.e.upwardpressurefromsoil
minusself-weightofbase.
WhenacolumntransmitsanaxialloadVEdandamomentMEd,thepunchingshearstressisgivenbythefollowingexpression:
vEd=(VEd,red/ud)[1+kMEdu/(VEd,redW)]
where u = theperimeterbeingconsidered k = acoefficientdependingontheratioofthecolumndimensionsshowninFigure8.2
andTable8.1 W = W1
Forasquarecolumnandageneralperimeteratriwithlengthui:
2+ 2c2
W1= + ri ric1 c2
c12
c1+ 4 ri 2 + p
ThepunchingshearresistancevRd,cgiveninSection8.4maybeenhancedforcolumnbasesbymultiplyingtheExpressionsby2d/a,whereaisthedistanceoftheperimeterconsideredfromtheperipheryofthecolumn.
Loadedarea
y
d
y≥arctan(0.5)
Figure 8.11Depth of control section in a footing with variable depth
BS EN 1992-1-1 6.4.2(6)
BS EN 1992-1-1 6.4.4(2)
BS EN 1992-1-1 Exp. (6.51)
PD 6687-2 7.3.1
59
Torsion
Torsion
General
Torsionalresistanceshouldbeverifiedinelementsthatrelyontorsionforstaticequilibrium.Instaticallyindeterminatebuildingstructuresinwhichtorsionarisesfromconsiderationofcompatibilityandthestructureisnotdependentontorsionforstability,itwillnormallybesufficienttorelyondetailingrulesforminimumreinforcementtosafeguardagainstexcessivecracking,withouttheexplicitconsiderationoftorsionatULS.
InEurocode2,torsionalresistanceiscalculatedbymodellingallsectionsasequivalentthin-walledsections.Complexsections,suchasT-sectionsaredividedintoaseriesofsub-sectionsandthetotalresistanceistakenasthesumoftheresistancesoftheindividualthin-walledsub-sections.
Thesamestrut inclinationy shouldbeusedformodellingshearandtorsion.The limits forcotynotedinSection7forshearalsoapplytotorsion.
Torsional resistances
Thedesigntorsionalresistancemoment
TRd,max=2vacw fcdAktef,isiny cosy
where v = 0.6[1–(fck/250)] Ak = areaenclosedbythecentrelinesofconnectingwallsincludingtheinnerhollow
area(seeFigure9.1) tef,i = effectivewallthickness(seeFigure9.1).ItmaybetakenasA/ubutshouldnotbe
takenaslessthantwicethedistancebetweenedge (theoutsidefaceofthe member) andcentreofthelongitudinalreinforcement.Forhollowsectionstherealthicknessisanupperlimit
y = angleofthecompressionstrut acw= coefficienttakingaccountofthestateofstressinthecompressionchord(seeTable7.2)
= 1 fornon-prestressedstructures
= (1+scp/fcd)for0<scp≤0.25fcd
= 1.25for0.25fcd<scp≤0.5fcd
= 2.5(1–scp/fcd)for0.5fcd<scp<1.0fcd
where scp=meancompressivestress,measuredpositive,intheconcreteduetothedesign
axialforce.
scp should be obtained by averaging it over the concrete section taking account of thereinforcement.Thevalueofscpneednotbecalculatedatadistancelessthan0.5dcotyfromtheedgeofthesupport.
BS EN 1992-1-1 6.3.1
BS EN 1992-1-1 6.3.2
BS EN 1992-2 6.3.2 (104)
BS EN 1992-26.2.3(103) & NA
9
9.1
9.2
60
Centreline
Cover
Outeredgeofeffectivecross-section,circumference,u
tef
zi
TEd
tef/2
Figure 9.1Notations used in Section 9
ThetorsionalresistanceofasolidrectangularsectionwithshearreinforcementontheouterperipheryTRd,maxmaybededucedfromthegeneralexpression,assumingteff=A/u:
TRd,max=2vacw fcdk2b3sinycosy
where k2 = coefficientobtainedfromTable9.1 b = breadthofthesection(<h,depthofsection)
Table 9.1Values of k2
h/b 1 2 3 4
k2 0.141 0.367 0.624 0.864
Torsionalresistancegovernedbytheareaofclosedlinksisgivenby:
TRd=Asw 2Akcotyfywd/s
where Asw = areaoflinkreinforcement fyw,d = designstrengthofthelinkreinforcement s = spacingoflinks
Therequiredareaoflongitudinalreinforcementfortorsion,SAsl,maybecalculatedfrom:
SAslfyd=TEdukcoty/(2Ak)
where TEd = applieddesigntorsion uk = perimeteroftheareaAk
Incompressivechords,thelongitudinalreinforcementmaybereducedinproportiontotheavailablecompressiveforce.Intensilechords,thelongitudinalreinforcementfortorsionshouldbeaddedtotheotherreinforcement.Thelongitudinalreinforcementshouldgenerallybedistributedoverthelengthofsidezi ,(sidelengthofwallidefinedbythedistancebetweentheintersectionpointswiththeadjacentwalls),butforsmallersectionsitmaybeconcentratedattheendsofthislength.
Bonded prestressing tendons can be taken into account limiting their stress increase toDsp≤500MPa.Inthatcase,SAslfydinExpression(6.28)isreplacedbySAslfyd+ApDsp.
ENV 1992-1-1 Exp. (4.43)[21]
BS EN 1992-2Exp. (6.28)
BS EN 1992-26.3.2(103)
BS EN 1992-1-1 fig. 6.11
61
Torsion
9.3 Combined torsion and shear
Insolidsectionsthefollowingrelationshipshouldbesatisfied:
(TEd/TRd,max)+(VEd/VRd,max)≤1.0
where TRd,max = designtorsionalresistancemoment = 2vacw fcdAktef,isinycosyasinSection9.2.
VRd,max = maximumdesignshearresistance =acwbw z v1 fcd(coty+cota)/(1+cot2y)asinSection7.3.2.
The effects of torsion and shear for both hollow and solid members may be superimposed,assumingthesamevalueforthestrutinclinationy.ThelimitsforygiveninSection7.3.2arealsofullyapplicableforthecaseofcombinedshearandtorsion.
For box sections, each wall should be verified separately, for the combination of shear forcesderivedfromshearandtorsion(Figure9.2).
a) Torsion b) Shear c) Combination
+ =
Figure 9.2Internal actions combination within the different walls of a box section
BS EN 1992-2 Exp. (6.29)
BS EN 1992-2 6.3.2 (102)
BS EN 1992-2 fig. 6.104
62
10
10.1
10.1.1
10.1.2
Strut-and-tie models, bearing zones and partially loaded areas
Design with strut-and-tie models
Struts
The design strength for a concrete strut in a region with transverse compressive stress or notransversestressmaybecalculatedfromthefollowingExpression(seeFigure10.1).
sRd,max=fcd= 0.85 fck / 1.5
Figure 10.1Design strength of concrete
struts without transverse tension
sRd,maxsRd,max
Figure 10.2Design strength of concrete
struts with transverse tension
sRd,maxsRd,max
Thedesignstrengthforconcretestrutsshouldbereducedincrackedcompressionzonesand,unlessamorerigorousapproachisused,maybecalculatedfromthefollowingExpression(seeFigure10.2).
sRd,max=0.6 (1–fck/250) fcd
where fcd= 1.0 fck/ 1.5
Ties
Reinforcementrequiredtoresisttheforcesattheconcentratednodesmaybesmearedoveralength(seeFigure10.3).Whenthereinforcementinthenodeareaextendsoveraconsiderablelength of an element, the reinforcement should be distributed over the length where thecompressiontrajectoriesarecurved(tiesandstruts).Thetensileforce,T,maybeobtainedby:
Forpartialdiscontinuityregions(■■ b ≤H/2)T=(b–a)F/4bForfulldiscontinuityregions(■■ b>H/2)T=(1–0.7a/h)F/4
BS EN 1992-1-16.5.2
BS EN 1992-1-1fig. 6.23
BS EN 1992-1-1fig. 6.24
BS EN 1992-1-16.5.3
63
Strut-and-tiemodels,bearingzonesandpartiallyloadedareas
10.1.3
a) Partial discontinuity b) Full discontinuity
bef
bef = 0.5H + 0.65a; aA h
a
b
z = h/2 h = H/2
F
F
h = bDiscontinuity region
Continuity region
Discontinuity region
H
bef
bef = b
a
b
F
F
Figure 10.3Parameters for the determination of transverse tensile forces in a compression field with smeared reinforcement
Nodes
Therulesfornodesalsoapplytoregionswhereconcentratedforcesaretransferredinamemberandwhicharenotdesignedbythestrut-and-tiemethod.Theforcesactingatnodesshouldbeinequilibrium.Transversetensileforcesperpendiculartoaninplanenodeshouldbeconsidered.
The dimensioning and detailing of concentrated nodes are critical in determining theirloadbearing resistance.Concentrated nodes may develop, for example, where point loads areapplied, at supports, in anchorage zones with concentration of reinforcement or prestressingtendons,atbendsinreinforcingbars,andatconnectionsandcornersofmembers.
Thedesignvaluesforthecompressivestresseswithinnodesmaybedeterminedinthreeways:
Incompressionnodeswherenotiesareanchoredatthenode(seeFigure10.4)■■
sRd,max= 1.0 (1–fck/250) fcd
where sRd,max = maximumstresswhichcanbeappliedattheedgesofthenode fcd = 0.85 fck/ 1.5
sRd,2 sRd,3
sRd,1
s c,0
a2
a3
a1
Fcd,1 = Fcd,1r + Fcd,l
Fcd,2
Fcd,3
Fcd,0
Fcd,1l Fcd,1r
Figure 10.4Compression node without ties
BS EN 1992-1-1 fig 6.25
BS EN 1992-1-1 6.5.4
BS EN 1992-1-1fig. 6.26
64
Incompression–tensionnodeswithanchoredtiesprovidedinonedirection(seeFigure10.5)■■
sRd,max= 0.85 (1–fck/250) fcd
where sRd,maxisthemaximumofsRd,1andsRd,2
fcd= 0.85 fck/ 1.5
sRd,1
sRd,2
s0
su
s0
Ftd
a1
lbd
Fcd,1
Fcd,2
R 2s0
a2
Figure 10.5Compression–tension node with reinforcement provided in one direction
Incompression–tensionnodeswithanchoredtiesprovidedinmorethanonedirection(see■■
Figure10.6),
sRd,max= 0.75 (1–fck/250) fcd
where
fcd= 0.85 fck/ 1.5
sRd,max
Ftd,1
Ftd,2
Fcd
Figure 10.6Compression–tension node with reinforcement provided in two directions
BS EN 1992-1-1fig. 6.27
BS EN 1992-1-1fig. 6.28
65
Strut-and-tiemodels,bearingzonesandpartiallyloadedareas
Theanchorageofthereinforcement incompression-tensionnodesstartsatthebeginningofthenode;inthecaseofasupportanchorage,startingatitsinnerface(seeFigure10.5).Theanchoragelengthshouldextendovertheentirenodelength.Incertaincases,thereinforcementmayalsobeanchoredbehindthenode.
Partially loaded areasForauniformdistributionofloadonanareaAc0(seeFigure10.7)theconcentratedresistanceforcemaybedeterminedasfollows:
FRdu = Ac0 fcd (Ac1 / Ac0)0.5 ≤ 3.0 fcd Ac0
where Ac0= loadedarea, Ac1= maximumdesigndistributionareawithasimilarshapetoAc0
fcd = 0.85 fck/ 1.5
ThedesigndistributionareaAc1requiredfortheresistanceforceFRdushouldcorrespondtothefollowingconditions:
Theheightfortheloaddistributionintheloaddirectionshouldcorrespondtothe■■
conditionsgiveninFigure10.7.Thecentreofthedesigndistributionarea■■ Ac1shouldbeonthelineofactionpassingthroughthecentreoftheloadareaAc0.Ifthereismorethanonecompressionforceactingontheconcretecross-section,the■■
designeddistributionareasshouldnotoverlap.
Reinforcement should be provided to resist the tensile forces due to the effect of actions,therulesforstrutandtiemaybeused.
Transverse tensile forces can arise in the localised area near a concentrated load and alsofrom any further spread of load outside the localised area.The strut-and-tie model usedshould account for both of these potential sources of transverse tensile forces FurtherguidanceandbackgroundaregivenbyHendy&Smith[20].
Line of action
b1
Ac1
Ac0
d1
hR (b2 – b1) and
b2A 3b1
d2A 3d1
R (d2 – d1)
h
Figure 10.7Design distribution for partially loaded areas
10.2 BS EN 1992-1-1 6.7
PD 6687-27.5
BS EN 1992-1-1fig. 6.29
66
10.3 Bearing zones of bridges
Forbearingzonesofbridges,Section10.2forpartiallyloadedareasshouldbeused,notingthefollowing.
ForconcreteclassesequaltoorhigherthanC55/67,theconcentratedresistanceforceshouldbecalculatedusingthefollowingExpression:FRdu = Ac0 fcd (0.46 fck 2/3) / (1 + 0.1 fck) x (Ac1 / Ac0)0.5 ≤ 3.0 Ac0 fcd (0.46 fck) / (1 + 0.1 fck
2/3)
Thedistancefromtheedgeoftheloadedareatothefreeedgeoftheconcretesectionshouldnotbelessthan1/6ofthecorrespondingdimensionoftheloadedareameasuredinthesamedirection.Innocaseshouldthedistancetothefreeedgebetakenaslessthan50mm.
Inordertoavoidedgesliding,uniformlydistributedreinforcementparalleltotheloadedfaceshouldbeprovidedtothepointatwhichlocalcompressivestressesaredispersed.Thispointisdeterminedbydrawingalineatanangle,y(30°),tothedirectionofloadapplicationfromtheedgeofthesectiontointersectwiththeoppositeedgeoftheloadedsurface,asshowninFigure10.8.Thereinforcementprovidedtoavoidedgeslidingshouldbeadequatelyanchored.
Figure 10.8Edge sliding mechanism
FRdu
y
Thereinforcementprovidedinordertoavoidedgesliding(Ar)shouldbecalculatedinaccordancewiththeexpressionArfyd≥FRdu/2.
BS EN 1992-2 fig. J.107
BS EN 1992-2J.104.1 (103)
BS EN 1992-2J.104.1 (102)
BS EN 1992-2J.104.1 (104)
67
Prestressedmembersandstructures
Prestressed members and structures
General
Thesectionprovidesguidancethatisspecifictoprestressedconcreteusingstressedtendons.Ingeneral,prestressisintroducedintheactioncombinationsdefinedinBSEN1990aspartoftheloadingcasesanditseffectsshouldbeincludedintheappliedinternalmomentandaxialforce.
The contribution of the prestressing tendons to the resistance of the section should belimited to their additional strength beyond prestressing.This requirement is most simplyachievedbytreatingthesecondaryeffectsofprestressasanappliedaction(i.e.aload),whilstomittingtheprimaryeffectsofthedesignprestressingforce.Thismaybecalculatedassumingthattheoriginofthestress–strainrelationshipofthetendonsisdisplacedbytheeffectsofprestressing.
Brittle fracture
Brittlefailureofthemembercausedbyfailureofprestressingtendonsshouldbeavoidedbyusingoneofthreemethodsgivenbelow .
Verification
Verifytheloadcapacityusingareducedareaofprestressasfollows:
Calculatetheappliedbendingmomentduetothefrequentcombinationofactions■■ Mfreq .Determinethereducedareaofprestress,■■ Ap,Red,thatresultsinthetensilestressreachingfctmattheextremetensionfibrewhenthesectionissubjecttothebendingmoment
calculatedabove.
Ap,Red=(Mfreq/z–fctm)/[sp(1/Ac+e/z)]
where z = sectionmodulus fctm = meanvalueofconcretecylindercompressivestrength sp = stressintendonsjustpriortocracking Ac = areaofconcrete e = eccentricityofthetendons
FurtherguidanceisgivenbyHendy&Smith[20]
Usingthisreducedareaofprestress,calculatetheultimateflexuralcapacity.Itshouldbe■■
ensuredthatthisexceedsthebendingmomentduetothefrequentcombination.RedistributionofinternalactionswithinthestructuremaybetakenintoaccountforthisverificationandtheultimatebendingresistanceshouldbecalculatedusingthematerialpartialfactorsforaccidentaldesignsituationsgiveninTable2.9.
Assumingthereisnoconventionalreinforcementthen:
Mfreq≥(fctmzs)/[(zs/z)–[sp(1/Ac+e/z)/fp0.1k ]]
where zs = leverarmfortheprestress,whereAp,Redhasbeenusedtodeterminethe
accidentalultimatelimitstate. fctm= meanvalueofconcretecylindercompressivestrength sp = stressintendonsjustpriortocracking
11
11.1
11.2
11.2.1
BS EN 1992-26.1(109)
68
Ac = areaofconcrete e = eccentricityofthetendons
FurtherguidanceisgivenbyHendy&Smith[20]
Minimum provision
The minimum reinforcement area, As,min, is given below. Reinforcing steel provided for otherpurposesmaybeincludedinAs,min.
As,min=Mrep/(zsfyk)
where Mrep= crackingbendingmomentcalculatedusinganappropriatetensilestrength,
fctk,0.05 attheextremetensionfibreofthesection,ignoringanyeffectofprestressing.AtthejointofsegmentalprecastelementsMrepshouldbeassumedtobezero
zs = leverarmattheultimatelimitstaterelatedtothereinforcingsteel
Thisminimumreinforcementsteelareashouldbeprovidedinregionswheretensilestressesoccurintheconcreteunderthecharacteristiccombinationofactions.Inthischeckthesecondaryeffectsofprestressingshouldbeconsideredandtheprimaryeffectsshouldbeignored.
Forpretensionedmembers,Expression(6.101a)shouldbeappliedusingoneofthealternativeapproachesdescribedbelow:
Tendonswithconcretecoveratleast■■ 1.0 timestheminimumspecifiedinFigure4.1areconsideredaseffectiveinAs,min.Avalueofzsbasedontheeffectivestrandsisusedintheexpressionandfykisreplacedwithfp0.1k.
Tendonssubjecttostresseslowerthan0.6■■ fpkafterlossesunderthecharacteristiccombinationofactionsareconsideredasfullyactive.Inthiscasethefollowingrequirementshouldbemet.
As,minfyk+ApDsp≥Mrep/z
where Dsp=smallerof0.4 fptkand500MPa
Toensureadequateductilitytheminimumreinforcingsteelarea■■ As,min,incontinuousbeamsshouldextendtotheintermediatesupportofthespanconsidered.Howeverthisextensionisnot necessary if, at the ultimate limit state, the resisting tensile capacity provided byreinforcingandprestressingsteelabovethesupports, calculated with the characteristicstrength fyk and fp0.1k respectively, is less than the resisting compressive capacity of thebottomflange.Thismeansthatthefailureofthecompressivezoneisnotlikelytooccur,andcanbeassessedasfollows:
Asfyk+ 1.0 Apfp0,1k<tinfb0 1.0 fck
where tinf = thethicknessofthebottomflangeofthesection.IncaseofT-sections,tinfis
takenasequaltob0 b0 = thewidthofthebottomflangeofthesection As = theareaofreinforcedsteelinthetensilezoneattheultimatelimitstate Ap = theareaofprestressingsteelinthetensilezoneattheultimatelimitstate
Inspection
Agreementofanappropriateinspectionregimewiththerelevantnationalauthorityonthebasisofsatisfactoryevidence.
11.2.2
11.2.3
BS EN 1992-2 Exp. (6.101a)
BS EN 1992-2 6.1(110)
BS EN 1992-2 Exp. (6.101b)
BS EN 1992-2 Exp. (6.102)
69
Prestressedmembersandstructures
Prestressing force during tensioning
Maximum stressing force
Theforceappliedtoatendon,Pmax(i.e.theforceattheactiveendduringtensioning)shallnotexceedthefollowingvalue:
Pmax=Apsp,max
where
Ap = cross-sectionalareaofthetendon sp,max = maximumstressappliedtothetendon = MIN{ 0.8 fpk; 0.9 fp0,1k}
Overstressingispermittediftheforceinthejackcanbemeasuredtoanaccuracyof±5%ofthefinalvalueoftheprestressingforce.InsuchcasesthemaximumprestressingforcePmaxmaybeincreasedto 0.95 fp0.1kAp(e.g.fortheoccurrenceofunexpectedlyhighfrictioninlong-line
pretensioning). Forpre-tensioningthisrelaxationisintendedtobeusedonlywherethereare unforeseenproblemsduringconstruction.
Theconcretecompressivestressinthestructureresultingfromtheprestressingforceandotherloadsactingatthetimeoftensioningorreleaseofprestress,shouldbelimitedto:
sc≤0.6fck(t)
where
fck(t) = characteristiccompressivestrengthoftheconcreteattimetwhenitissubjectedtotheprestressingforce
Forpretensionedelementsthestressatthetimeoftransferofprestressmaybeincreasedto0.7 fck(t),ifitcanbejustifiedbytestsorexperiencethatlongitudinalcrackingisprevented.
Ifthecompressivestresspermanentlyexceeds0.45fck(t)thenon-linearityofcreepshouldbetakenintoaccount.
Prestress force
ThevalueoftheinitialprestressforcePm0(x)(attimet=t0)appliedtotheconcreteimmediatelyaftertensioningandanchoring(post-tensioning)oraftertransferofprestressing(pre-tensioning)isobtainedbysubtractingfromtheforceattensioningPmaxtheimmediatelossesDPi(x)andshouldnotexceedthefollowingvalue:
Pm0(x)=Apspm0(x)
where
spm0(x) = stressinthetendonimmediatelyaftertensioningortransfer = MIN{ 0.75 fpk; 0.85 fp0,1k}
Atagiventimetanddistancex(orarclength)fromtheactiveendofthetendonthemeanprestressforcePm,t(x)isequaltothemaximumforcePmaximposedattheactiveend,minustheimmediatelossesandthetimedependentlosses:
Pm,t(x)=Pm0(x)-DPc+s+r(x).
where Pm,t(x) = meanvalueoftheprestressforceatthetimet>t0andshouldbe
determinedwithrespecttotheprestressingmethod DPc+s+r(x) = changeinprestressduetotheresultofcreep,shrinkageoftheconcrete
andthelongtermrelaxationoftheprestressingsteel
Absolutevaluesareconsideredforallthelosses.
11.3
11.3.1
11.3.2
BS EN 1992-1-1 5.10.2.1
BS EN 1992-1-1 5.10.2.2(5)
BS EN 1992-1-1 5.10.3(2)
BS EN 1992-1-1 5.10.3(1)&(4)
70
Immediate losses
WhendeterminingtheimmediatelossesDPi(x)thefollowingimmediateinfluencesshouldbeconsideredforpre-tensioningandpost-tensioningwhererelevant:
Lossesduetoelasticdeformationofconcrete,■■ DPel.
Forpre-tensioning:
DPel(x)=ApEpsc(x)/Ecm(t)
where Ep = modulusofelasticityofprestressingsteel Ecm(t) = modulusofelasticityofconcreteattime,t sc(x) = stressintheconcreteadjacenttothetendonattransfer
Forpost-tensioning:DPel=ApEpS(jDsc(t)/Ecm(t))
where Dsc(t)=variationofstressintheconcreteatthecentreofgravityofthetendonsapplied
attimet j =(n–1)/2nwhenconsideringlossesbeforestressing.Asanapproximationjmaybe
takenas1/2 =1forthevariationsduetopermanentactionsappliedafterprestressing n =numberofidenticaltendonssuccessivelyprestressed.
Lossesduetoshorttermrelaxation,■■ DPr (e.g.lossduetorelaxationoftheprestressing duringtheperiodwhichelapsesbetweenthetensioningofthetendonsandprestressingof theconcrete).
■■■ Lossesduetofriction,DPμ(x),inpost-tensionedtendonsmaybeestimatedfrom:
D Pμ(x)=Pmax(1−e–μ(y+kx))
where y = sumoftheangulardisplacementsoveradistancex(irrespectiveofdirectionorsign) μ = coefficientoffrictionbetweenthetendonanditsduct k = unintentionalangulardisplacementforinternaltendons(perunitlength) x = distancealongthetendonfromthepointwheretheprestressingforceisequalto
Pmax(theforceattheactiveendduringtensioning)
ThevaluesμandkaregivenintherelevantEuropeanTechnicalApproval.Intheabsenceofdatagiven inaEuropeanTechnicalApprovalthevaluesforμgiven inTable11.1maybeassumed.Unintendedangulardisplacementsforinternaltendonswillgenerallybeintherange0.005<k <0.01permetre.
Table 11.1Coefficients of friction, μ, for post-tensioned internal tendons and external unbonded tendons
Tendon type Internal tendonsa
External unbonded tendons
Steel duct: non-lubricated
HDPE duct: non-lubricated
Steel duct: lubricated
HDPE duct: lubricated
Cold drawn wire 0.17 0.25 0.14 0.18 0.12
Strand 0.19 0.24 0.12 0.16 0.10
Deformed bar 0.65 – – – –
Smooth round bar 0.33 – – – –
Key
aFortendonswhichfillabouthalfoftheduct
11.3.3
BS EN 1992-1-1 5.10.3(3)
BS EN 1992-1-1 5.10.5.1(2)
BS EN 1992-1-1 5.10.5.2(1)
BS EN 1992-1-1 5.10.5.2(2)&(3)
BS EN 1992-1-1 table 5.1
71
Prestressedmembersandstructures
Lossesduetoanchorageslip,■■ DPsl, whichareavailablefromtheEuropeanTechnical Approval.Lossesduetofrictionatthebends(inthecaseofcurvedwiresorstrands).■■
Time-dependent losses of prestressAsimplifiedmethodtoevaluatetimedependentlossesatlocationxunderthepermanentloadsisasfollows:
ApDsp,c+s+r DPc+s+r = = Ap
ecsEp+ 0.8Dspr +Ep
Ecm
h (t,t0)sc,QP
(1 + )1 + Ac
zcpIc
Ep Ap
Ecm Ac
2 [1 + 0.8 h (t,t0)]
where Ap = areaofalltheprestressingtendonsatthelocationx Dsp,c+s+r= absolutevalueofthevariationofstressinthetendonsduetocreep, shrinkageandrelaxationatlocationx,attimet ecs = estimatedshrinkagestrain,inabsolutevalue Ep = modulusofelasticityfortheprestressingsteel Ecm = modulusofelasticityfortheconcrete Dspr = absolutevalueofthevariationofstressinthetendonsatlocationx,at timet,duetotherelaxationoftheprestressingsteel.Itisdeterminedfor astressofsp=sp(G +Pm0+c2Q),whichistheinitialstressinthetendons duetoinitialprestressandquasi-permanentactions h (t,t0) = creepcoefficientatatimetandloadapplicationattimet0 sc,QP = stressintheconcreteadjacenttothetendons,duetoself-weightandinitial
prestressandotherquasi-permanentactionswhererelevant.Thevalueofsc,QPmaybetheeffectofpartofself-weightandinitialprestressortheeffectofafullquasi-permanentcombinationofactions(sc(G +Pm0+c2Q)),dependingonthestageofconstructionconsidered
Ac = areaoftheconcretesection Ic = secondmomentofareaoftheconcretesection zcp =distance between the centre of gravity of the concrete section and the
tendons
Compressive stresses and the corresponding strains should be used with a positive sign.ThisExpressionappliesforbondedtendonswhenlocalvaluesofstressesareusedandforunbondedtendonswhenmeanvaluesofstressesareused.Themeanvaluesshouldbecalculatedbetweenstraight sections limited by the idealised deviation points for external tendons or along theentirelengthincaseofinternaltendons.
Effects of prestressing at ultimate limit state
IngeneralthedesignvalueoftheprestressingforcemaybedeterminedfromPd,t(x)=gP, Pm,t(x)
For prestressed members with permanently unbonded tendons, it is generally necessary totakethedeformationofthewholememberintoaccountwhencalculatingtheincreaseofthestressintheprestressingsteel.Ifnodetailedcalculationismade,itmaybeassumedthattheincrease of the stress from the effective prestress to the stress in the ultimate limit state is
100MPaunlessthetendonisoutwithbdfromthetensionface,inwhichcaseDsp,ULS=0.b =0.1ford≥1000mm =0.25ford≤500mmThevalueofbmaybeinterpolatedforthevaluesofdbetween500mmand1000mm.
Ifthestressincreaseinexternaltendonsiscalculatedusingthedeformationstateoftheoverallmember,non-linearanalysisshouldbeused.
11.3.4
11.3.5
BS EN 1992-1-1 5.10.6
BS EN 1992-1-1 5.10.8 & NA
BS EN 1992-2 5.10.8 (103)
72
FatigueVerification conditions
Becauseofthehighliveloadtodeadloadratio,deckslabsarelikelytobeamongsttheelementsmostaffectedbyfatiguecalculations.However,testsshowthattheactualstressrangesinthereinforcementinthesearemuchlowerthantheconventionalelasticcalculationssuggest.Becauseofthis,theNAtoBSEN1992-2identifiescaseswherefatigueassessmentisnotrequiredandprovidesconservativerules.
Afatigueverificationisgenerallynotnecessaryforthefollowingstructuresandstructuralelements:
Footbridges,withtheexceptionofstructuralcomponentsverysensitivetowindaction.■■
Buriedarchandframestructureswithaminimumearthcoverof1mand1.5mforroad■■
andrailwaybridges.Foundations.■■
Piersandcolumnswhicharenotrigidlyconnectedtosuperstructures.■■
Retainingwallsofembankmentsforroadsandrailways.■■
Abutmentsofroadandrailwaybridgeswhicharenotrigidlyconnectedtosuperstructures,■■
excepttheslabsofhollowabutments.Prestressingandreinforcingsteel,inregionswhere,underthefrequentloadcombinationof■■
actionsandPkonlycompressivestressesoccurattheextremeconcretefibres.
Fatigue verification for road bridges is not necessary for the local effects of wheel loadsapplieddirectlytoaslabspanningbetweenbeamsorwebsprovidedthat:
Theslabdoesnotcontainweldedreinforcementorreinforcementcouplers.■■
Theclearspantooveralldepthratiooftheslabdoesnotexceed18.■■
Theslabactscompositelywithitssupportingbeamsorwebs.■■
Either:■■
theslabalsoactscompositelywithtransversediaphragms;or
thewidthoftheslabperpendiculartoitsspanexceedsthreetimesitsclearspan.
Internal forces and stresses for fatigue verification
Thestresscalculationshallbebasedontheassumptionofcrackedcross-sectionsneglectingthetensilestrengthofconcretebutsatisfyingcompatibilityofstrains.
Theeffectofdifferentbondbehaviourofprestressingandreinforcingsteelshallbetakenintoaccountbyincreasingthestressrangeinthereinforcingsteelcalculatedundertheassumptionofperfectbondbythefactor,n,givenby
As + Ap
As + Ap n =
j cfs/fpm
where: As = areaofreinforcingsteel
Ap = areaofprestressingtendonortendons
fs = largestdiameterofreinforcement
fp = diameterorequivalentdiameterofprestressingsteel
= 1.6√−
APforbundles
= 1.75fwireforsingle7-wirestrandswherefwireisthewirediameter
= 1.20fwireforsingle3-wirestrandswherefwireisthewirediameter
j = ratioofbondstrengthbetweenbondedtendonsandribbedsteelinconcrete.ThevalueissubjecttotherelevantEuropeanTechnicalApproval.IntheabsenceofthisthevaluesgiveninTable12.1maybeused.
12 12.1
12.2
BS EN 1992-2 6.8.1(102)
BS EN 1992-2 NA 6.8.1(102)
BS EN 1992-1-1 6.8.2
PD 6687-2 7.6.1
73
Fatigue
Table 12.1Ratio of bond strength, j , between tendons and reinforcing steel
Prestressing steel j
Pre-tensioned Bonded, post-tensioned
≤ C50/60 ≥ C70/85
Smooth bars and wires Notapplicable 0.3 0.15
Strands 0.6 0.5 0.25
Indented wires 0.7 0.6 0.30
Ribbed bars 0.8 0.7 0.35
NoteForintermediatevaluesbetweenC50/60andC70/85interpolationmaybeused.
Inthedesignoftheshearreinforcementtheinclinationofthecompressivestrutsyfatmaybecalculatedusingastrut-and-tiemodelorinaccordancewithtan yfat = tan y ≤ 1.0
where
y = angleofcompressionstrutstothebeamaxisassumedinULSdesign(seeSection7.3.2).
Verification of concrete under compression or shear
S–N curves required to undertake a fatigue verification of concrete under compression orshearareunlikelytobeavailablefromNationalAuthorities.Intheabsenceofsuchdata,thesimplifiedapproachgiveninBSEN1992-2,AnnexNNmaybeusedforrailwaybridges,butnosuchoptionexistsforhighwaybridges.
The fatigue verification for concrete under compression may be assumed tobemet if thefollowingconditionissatisfied:
fcd,fat
sc,max≤ 0.5 + 0.45
fcd,fat
sc,min
where
sc,max= maximum compressive stress at a fibre under the frequent load combination(compressionmeasuredpositive)
sc,min = minimumcompressivestressatthesamefibrewheresc,maxoccurs.Ifsc,minisatensilestress,thensc,minshouldbetakenas0
fcd,fat = designfatiguestrengthofconcrete
fck = 0.85 bcc(t0)fcde1–
250n
fcd = 1.0 fck/ 1.5
bcc(t0)=coefficientforconcretestrengthatfirstloadapplication
■ =
bcc (t0) where = exp s 1 – 28t0
0.5
where t0 = timeofthestartofthecyclicloadingonconcreteindays s = 0.2forcementofstrengthClassesCEM42.5R,CEM52.5NandCEM52.5R(ClassR) = 0.25forcementofstrengthClassesCEM32.5R,CEM42.5(ClassN) = 0.38forcementofstrengthClassCEM32.5(ClassS)
Themaximumvaluefortheratiosc,max/fcd,fatisgiveninTable12.2.
12.3
PD 6687-27.6.2
BS EN 1992-1-1table 6.2
BS EN 1992-1-16.8.7(2)
74
Table 12.2Values for sc,max /fcd, fat
Concrete strength sc,max /fcd, fat
fck≤50MPa ≤0.9
fck>50MPa ≤0.8
For members not requiring design shear reinforcement for the ultimate limit state it may beassumedthattheconcreteresistsfatigueduetosheareffectswherethefollowingapply:
for ≥ 0:
≤ 0.5 + 0.45≤ 0.9 up to C50/60
≤ 0.8 greater than C55/67
VEd,min
VEd,max
VEd,max
VRd,c
VEd,min
VRd,c
for < 0:
≤ 0.5
VEd,min
VEd,max
VEd,max
VRd,c
VEd,min
VRd,c
where VEd,max =designvalueofthemaximumappliedshearforceunderfrequentload
combination VEd,min = isthedesignvalueoftheminimumappliedshearforceunderfrequentload
combinationinthecross-sectionwhereVEd,maxoccurs VRd,c = designvalueforshearresistanceaccordingtoSection7.2.1.
Limiting stress range for reinforcement under tension
Adequate fatigue resistance may be assumed for reinforcing bars under tension if the stressrange under the frequent cyclic load combined with the basic combination does not exceed70MPa forunweldedbarsand 35MPa forweldedbars.
For UK highway bridges, the values in Tables 12.3 and 12.4 may be used for straightreinforcement.ThesearebasedonbarsconformingtoBS4449.ForbarsnotconformingtoBS4449,therulesforbars>16mmdiametershouldbeusedforallsizesunlesstherangesforbars≤16mmdiametercanbejustified.
Table 12.3Limiting stress ranges – longitudinal bending for unwelded reinforcing bars in road bridges, MPa
Span m Adjacent spans loaded Alternate spans loaded
Bars ≤ 16 mm Bars > 16 mm Bars ≤ 16 mm Bars > 16 mm
≤ 3.5 150 115 210 160
5 125 95 175 135
10 110 85 175 135
20 110 85 140 110
30 to 50 90 70 110 85
100 115 90 135 105
≥ 200 190 145 200 155
Notes 1Intermediatevaluesmaybeobtainedbylinearinterpolation.
2ThistableappliestoslabsbutneedonlybeappliedtothoseslabsthatdonotconformtothecriteriagiveninSection12.1.
12.4
PD 6687-2table 2A
BS EN 1992-1-16.8.7(4)
BS EN 1992-1-16.8.6(1)
PD 6687-27.6.3
75
Fatigue
Table 12.4Limiting stress ranges – transverse bending for unwelded reinforcing bars in road bridges, MPa
Span m Bars ≤ 16 mm Bars > 16 mm
≤3.5 210 160
5 120 90
≥10 70 55
Notes1Intermediatevaluesmaybeobtainedbylinearinterpolation.
2ThistableappliestoslabsbutneedonlybeappliedtothoseslabsthatdonotconformtothecriteriagiveninSection12.1.
IfthestressrangelimitsexceedthevaluesgiveninTables12.3and12.4(e.g.forreinforcementoverthepier),fullfatiguechecksaretobecarriedoutusingthe‘damageequivalentstressrange’method,followingtheguidancegiveninAnnexNNofBSEN1992-2.Thestressrangesarecalculatedusing‘FatigueLoadModel3’,whichrepresentsafour-axlevehiclewithanallupweightof48tonnes.AnnexNNfurtherincreasesthisweightto84tonnesforintermediatesupportsand67tonnesforotherareas.
PD 6687-2table 2B
76
ServiceabilityGeneral
Thecommonserviceabilitylimitstatesconsideredare:
Stresslimitation.■■
Crackcontrol.■■
Deflectioncontrol.■■
Inthecalculationofstressesanddeflections,cross-sectionsshouldbeassumedtobeuncrackedprovidedthattheflexuraltensilestressdoesnotexceedfct,eff.Thevalueoffct,effmaybetakenasfctmorfctm,flprovidedthatthecalculationforminimumtensionreinforcementisalsobasedon the same value. For the purposes of calculating crack widths and tension stiffening fctmshouldbeused.
Stress limitation
Longitudinalcracksmayoccurifthestresslevelunderthecharacteristiccombinationofloadsexceedsacriticalvalue.Suchcrackingmayleadtoareductionofdurability.Intheabsenceofothermeasures,suchasanincreaseinthecovertoreinforcementinthecompressivezoneorconfinement by transverse reinforcement, it isrecommendedthat the compressive stress islimitedtoavalue 0.6 fckinareasexposedtoenvironmentsofexposureclassesXD,XFandXS(seeTable4.2).Inthepresenceofconfinementthemaximumstresslimitis 0.66 fck.
Ifthestressintheconcreteunderthequasi-permanentloadsislessthan 0.45 fck,linearcreepmay be assumed. If the stress in concrete exceeds 0.45 fck, non-linear creep should beconsidered(seeSection3.1.2).
For the appearance unacceptable cracking or deformation may be assumed to be avoidedif, under the characteristic combination of loads, the tensile stress in the reinforcement doesnotexceed 0.8 fyk.Wherethestress iscausedbyan imposeddeformation,thetensilestressshould not exceed 1.0 fyk.The mean value of the stress in prestressing tendons should not
exceed 0.75 fpk. Crack control (Section 13.4) and deflection (Section 13.6) should also be
checked.
Calculation of crack widths
Thecrackwidth,wk,maybecalculatedfromfollowingExpression:
wk=sr,max(esm–ecm)
where sr,max = maximumcrackspacing esm = meanstraininthereinforcementundertherelevantcombinationofloads,
includingtheeffectofimposeddeformationsandtakingintoaccounttheeffectsoftensionstiffening.Onlytheadditionaltensilestrainbeyondthestateofzerostrainoftheconcreteatthesamelevelisconsidered
ecm = meanstrainintheconcretebetweencracks
esm–ecmmaybecalculatedfromtheExpression:
fct,eff
rct,effss – kt
Es
(1 + ae rp,eff) ss
Es
0.6esm – ecm =
where ss = stressinthetensionreinforcementassumingacrackedsection.For
pretensionedmembers,ssmaybereplacedbyDsp,whichisthestressvariationinprestressingtendonsfromthestateofzerostrainoftheconcreteatthesamelevel
13 13.1
13.2
13.3
BS EN 1992-1-17.1
BS EN 1992-27.2(102) & NA
PD 6687-28.1.1
PD 6687-28.1.2
BS EN 1992-1-17.3.4
BS EN 1992-1-17.2(3)
BS EN 1992-1-17.2(5), NA
77
Serviceability
kt = factordependentonthedurationoftheload
= 0.6forshorttermloading
= 0.4forlongtermloading
ae = ratioEs/Ecm
rp,eff = (As+j12Ap' )/Ac,eff
where
Ap' = areaofpre-orpost-tensionedtendonswithinAc,eff.
Ac,eff = effectiveareaofconcreteintensionsurroundingthereinforcementorprestressingtendonsofdepth,hc,ef,wherehc,efisthelesserof2.5(h – d),(h – x)/3orh/2(seeFigure13.3).
j1 = adjustedratioofbondstrengthtakingintoaccountthedifferentdiametersofprestressingandreinforcingsteel:
= (j fs/fp)0.5
j = ratioofbondstrengthofprestressingandreinforcingsteel,accordingtoTable12.1
Ifonlyprestressingsteelisusedtocontrolcracking,j1=j 0.5
fs = largestbardiameterofreinforcingsteel
fp = equivalentdiameteroftendonaccordingtoSection12.2
Insituationswherebondedreinforcementisfixedatreasonablyclosecentreswithinthetensionzone(spacing≤5(c +f/2),themaximumfinalcrackspacingmaybecalculatedfromfollowingExpression(seeFigure13.1):
sr,max=k3c + k1k2k4f/rp,eff
where f = bar diameter.Where a mixture of bar diameters is used in a section, an equivalent
diameter,feq,shouldbeused where feq = (n1f1
2+n2f2)/(n1f1+n2f2) n1 = numberofbarsofdiameterf1 n2 = numberofbarsofdiameterf2 k3 = 3.4 c = covertothelongitudinalreinforcement. Thenominalcover,cnom,maybeused. k1 = coefficientwhichtakesaccountofthebondpropertiesofthebonded
reinforcement = 0.8forhighbondbars = 1.6forbarswithaneffectivelyplainsurface(e.g.prestressingtendons)
f
Concretetension surface
Crack spacing predictedby Expression (7.14)
Crack spacing predicted byExpression (7.11)
Actual crack width
Neutral axis
(h – x)
5(c + f/2)
c
w
Figure 13.1Crack width, w, at concrete surface relative to distance from bar
BS EN 1992-1-1fig. 7.2
BS EN 1992-1-1Exp. (7.11)
78
k4 = 0.425 k2 = coefficientwhichtakesaccountofthedistributionofstrain = 0.5forbending = 1.0forpuretension Forcasesofeccentrictensionorforlocalareas,intermediatevaluesofk2should
beusedwhichmaybecalculatedfromtherelation: k2 = (e1+e2)/(2e1) e1 = greatertensilestrainattheboundariesofthesectionconsidered,assessedon
thebasisofacrackedsection e2 = lessertensilestrainattheboundariesofthesectionconsidered,assessedonthe
basisofacrackedsection
Wherethespacingofthebondedreinforcementexceeds5(c+f/2)(seeFigure13.1)orwherethereisnobondedreinforcementwithinthetensionzone,anupperboundtothecrackwidthmaybefoundbyassumingamaximumcrackspacing:
sr,max=1.3(h – x)
Wheretheanglebetweentheaxesofprincipalstressandthedirectionofthereinforcement,formembersreinforcedintwoorthogonaldirections,issignificant(>15°),thenthecrackspacingsr,maxmaybecalculatedfromthefollowingexpression:
sr,max=1/(cosy/sr,max,y+siny/sr,max,z)
where y = anglebetweenthereinforcementinthe ydirectionandthedirectionofthe
principaltensilestress sr,max,y= crackspacingcalculatedinthey-direction sr,max,z= crackspacingcalculatedinthez-direction
Alimitingcalculatedcrackwidth wmax ,takingaccountoftheproposedfunctionandnatureofthestructureandthecostsoflimitingcracking,shouldbeestablished.Duetotherandomnatureof the cracking phenomenon, actual crack widths cannot be predicted. However, if the crackwidths calculated in accordance with the models given in BS EN 1992-2 are limited to thevaluesgiveninTable13.1,theperformanceofthestructureisunlikelytobeimpaired.
The decompression limit requires that all concrete within a certain distance of bondedtendons or their ducts should remain in compression under the specified loading. Thedistancewithinwhichallconcreteshouldremainincompressionshouldbetakenasthevalueofcmin,dur.WherethemosttensilefaceofasectionisnotsubjecttoXDorXSexposurebutanother face is, the decompression limit should require all tendons within 100 mm of asurface subject toXD orXS exposure to have a depth cmin,dur of concrete in compressionbetweenthemandsurfacessubjecttoXDorXSexposure.
Sincethedecompressionlimitof100mmislikelytobegreaterthanthecoverrequiredfordurability,thisintroducesananomaly.Forexample,only50mmofconcreteincompressionmight be deemed adequate to protect the tendons, whereas 60 mm of concrete incompressionplus40mmnotincompressionwouldnot,whichisclearlyillogical.Changingthedistancefromtherecommendedvalueof100mmtothecoverrequiredfordurability,cmin,dur,ismorelogical.
In some situations, such as structures cast against the ground, cnom will be significantlygreaterthanthecoverrequiredfordurability.Wheretherearenoappearancerequirementsitisreasonabletodeterminethecrackwidthatthecoverrequiredfordurabilityandverifythatitdoesnotexceedtherelevantmaximumcrackwidth.Thismaybedonebymultiplyingthecrackwidthdeterminedatthesurfaceby(cmin,dur,+Dcdev)/cnomtogivethecrackwidthat the cover required for durability, and verifying that it is not greater than wmax. Thisapproach assumes that the crack width varies linearly from zero at the bar. Given theaccuracyofcrackcalculationmethodsthissimplificationisconsideredreasonable.
BS EN 1992-2NA. NA.2.2
BS EN 1992-27.3.1(105) & NA
BS EN 1992-1-1Exp. (7.14)
PD 6687-2 8.2.1b)
PD 6687-2 8.2.2
79
Serviceability
13.4
Table 13.1Recommended values of wmax and relevant combination rules
Exposure classa Reinforced members and prestressed members without bonded tendons
Prestressed members with bonded tendons
Quasi-permanent load combinationb (mm)
Frequent load combinationb (mm)
X0, XC1 0.3c 0.2
XC2, XC3, XC4 0.3 0.2d
XD1, XD2, XD3 XS1, XS2, XS3
0.3 0.2e anddecompression
KeyaTheexposureclassconsidered,includingattransfer,appliestothemostsevereexposurethesurface
willbesubjecttoinservice.
bForthecrackwidthchecksundercombinationswhichincludetemperaturedistribution,theresultingmemberforcesshouldbecalculatedusinggrosssectionconcretepropertiesandself-equilibrating thermalstresseswithinasectionmaybeignored.
cForX0,XC1exposureclasses,crackwidthhasnoinfluenceondurabilityandthislimitissettoguaranteeacceptableappearance.Intheabsenceofappearanceconditionsthislimitmayberelaxed.
dFortheseexposureclasses,inaddition,decompressionshouldbecheckedunderthequasipermanentcombinationofloads.
e0.2appliestothepartsofthememberthatdonothavetobecheckedfordecompression.
Control of cracking
WheretheminimumreinforcementgivenbySection13.5isprovided,crackwidthsareunlikelytobeexcessiveif:
Forcrackingcausedpredominantlybyrestraint,thebarsizesgiveninTable13.2arenot■■
exceededwherethesteelstressisthevalueobtainedimmediatelyaftercracking(i.e.ssinSection13.5).Forcrackscausedmainlybyloading,eithertheprovisionsofTable13.2ortheprovisionsof■■
Table13.3arecompliedwith.Thesteelstressshouldbecalculatedonthebasisofacrackedsectionundertherelevantcombinationofactions.
Forpre-tensionedconcrete,wherecrackcontrolismainlyprovidedbytendonswithdirectbond,Tables13.2and13.3maybeusedwithastressequaltothetotalstressminusprestress.Forpost-tensionedconcrete,wherecrackcontrolisprovidedmainlybyordinaryreinforcement,thetablesmaybeusedwiththestressinthisreinforcementcalculatedwiththeeffectofprestressingforcesincluded.
Themaximumbardiametershouldbemodifiedasfollows:
Bending(atleastpartofsectionincompression):
fs = f*s ( fct,eff/2.9)kchcr
2 (h – d)
Tension(uniformaxialtension):
fs = f*s ( fct,eff/2.9) hcr/(8(h – d))
where fs = adjustedmaximumbardiameter fs = maximumbarsizegivenintheTable13.2 h = overalldepthofthesection hcr = depthofthetensilezoneimmediatelypriortocracking,consideringthe
characteristicvaluesofprestressandaxialforcesunderthequasi-permanentcombinationofactions
d = effectivedepthtothecentroidoftheouterlayerofreinforcement
BS EN 1992-2 &NA, table NA.2
BS EN 1992-1-1 7.3.3(2)
80
Whereallthesectionisundertensionh–distheminimumdistancefromthecentroidofthelayer of reinforcement to the face of the concrete (consider each face where the bar is notplacedsymmetrically).
Table 13.2Maximum bar diameters for crack control
Steel stress (MPa) Maximum bar size (mm) for crack widths of
0.4 mm 0.3 mm 0.2 mm
160 40 32 25
200 32 25 16
240 20 16 12
280 16 12 8
320 12 10 6
360 10 8 5
400 8 6 4
450 6 5 —
Table 13.3Maximum bar spacing for crack control
Steel stress (MPa) Maximum bar spacing (mm) for maximum crack widths of
0.4 mm 0.3 mm 0.2 mm
160 300 300 200
200 300 250 150
240 250 200 100
280 200 150 50
320 150 100 —
360 100 50 —
Minimum reinforcement areas of main bars
Ifcrackcontrolisrequired,aminimumamountofbondedreinforcementisrequiredtocontrolcrackinginareaswheretensionisexpected.TherequiredminimumareasofreinforcementAs,minmaybecalculatedasfollows.Inprofiledcross-sectionslikeT-beamsandboxgirders,minimumreinforcementshouldbedeterminedfortheindividualpartsofthesection(webs,flanges).
As,min=kckfct,effAct/ss
where Act = areaofconcretewithintensilezone.Thetensilezoneisthatpartofthesection
whichiscalculatedtobeintensionjustbeforeformationofthefirstcrack ss = absolutevalueofthemaximumstresspermittedinthereinforcement
immediatelyafterformationofthecrack.Thismaybetakenastheyieldstrengthofthereinforcement,fyk.Alowervaluemay,however,beneededtosatisfythecrackwidthlimitsaccordingtothemaximumbarsizeorspacingindicatedinTables13.2and13.3.
fct,eff = meanvalueofthetensilestrengthoftheconcreteeffectiveatthetimewhenthecracksmayfirstbeexpectedtooccur.
= fctmorlower( fctm(t))ifcrackingisexpectedearlierthan28days
Aminimumvalueof2.9MPashouldbetaken k = coefficientwhichallowsfortheeffectofnon-uniformself-equilibratingstresses,
whichleadtoareductionofrestraintforces = 1.0forwebswithh≤300mmorflangeswithwidthslessthan300mm,
intermediatevaluesmaybeinterpolated
13.5
BS EN 1992-1-1table 7.3N
BS EN 1992-1-17.3.2(1)
BS EN 1992-27.3.2(102)
BS EN 1992-1-1table 7.2N
BS EN 1992-1-1Exp. (7.1)
BS EN 1992-27.3.2(105)
81
Serviceability
= 0.65forwebswithh≥800mmorflangeswithwidthsgreaterthan800mm,intermediatevaluesmaybeinterpolated
kc = coefficientwhichtakesaccountofthestressdistributionwithinthesectionimmediatelypriortocrackingandofthechangeoftheleverarm:
= 1.0forpuretension. = 0.4forpurebending. = 0.4[1–(sc/(k1(h/h*)fct,eff))]≤1forrectangularsectionsandwebsofbox
sectionsandT-sections. = 0.9Fcr/(Actfct,eff)≥0.5forflangesofboxsectionsandT-sections. sc = meanstressoftheconcreteactingonthepartofthesectionunderconsideration. = NEd/bh NEd = axialforceattheserviceabilitylimitstateactingonthepartofthecross-section
underconsideration(compressiveforcepositive).NEdshouldbedeterminedconsideringthecharacteristicvaluesofprestressandaxialforcesundertherelevantcombinationofactions
h* = MIN{h;1.0} k1 = coefficientconsideringtheeffectsofaxialforcesonthestressdistribution: = 1.5ifNEdisacompressiveforce = 2h*/3hifNEdisatensileforce Fcr = absolutevalueofthetensileforcewithintheflangeimmediatelypriortocracking
duetothecrackingmomentcalculatedwithfct,eff
SeealsoSection15.2.1forasimplifiedmethodofcalculatingminimumareaofsteel.
Inflangedcross-sectionslikeT-beamsandboxgirders,thedivisionintopartsshouldbeasindicatedinFigure13.2.
sc, web
sc, flange
fct,eff fct,eff
Flange Flange
Web
Sflange
Sm
Sweb
Web Flange
a) Components b) Stresses
Figure 13.2Example for a division of a flanged cross-section for analysis of cracking
Bondedtendonsinthetensionzonemaybeassumedtocontributetocrackcontrolwithinadistance≤150mmfromthecentreofthetendon.Thismaybetakenintoaccountbyincludingthetermj1Ap
' DpintheExpressionabovetogive:
As,min=(kckfct,effAct–j1Ap' Dsp)/ss
where Ap
' = areaofpre-orpost-tensionedtendonswithinAc,eff Ac,eff = effectiveareaofconcreteintensionsurroundingthereinforcementor
prestressingtendonsofdepth,hc,ef hc,ef = MIN{2.5(h – d);(h – x)/3;h/2}(seeFigure13.3) j1 = adjustedratioofbondstrengthtakingintoaccountthedifferentdiametersof
prestressingandreinforcingsteel =(j fs/fp)0.5
= j 0.5ifonlyprestressingsteelisusedtocontrolcracking j = ratioofbondstrengthofprestressingandreinforcingsteel,accordingto
Table13.4
BS EN 1992-2fig. 7.101
BS EN 1992-1-1 7.3.2(3)
82
fs = largestbardiameterofreinforcingsteel fp = equivalentdiameteroftendon = 1.6Ap
0.5forbundles = 1.75fwireforsingle7wirestrandswherefwireisthewirediameter = 1.20fwireforsingle3wirestrandswherefwireisthewirediameter Dsp = stressvariationinprestressingtendonsfromthestateofzerostrainofthe
concreteatthesamelevel
Level of steel centroid
Effective tension area, Ac,eff
Effective tension area, Ac,eff
Effective tension area for upper surface, Act,eff
Effective tension area for lower surface, Acb,eff
e2 = 0
e2 = 0
a) Beam
b) Slab
c) Member in tension
e1
e1
e2
e1
hc,ef
hc,ef
hc,ef
hc,ef
h
h d
h d d
x
d
x
Figure 13.3Effective tension area (typical cases)
In prestressed members no minimum reinforcement is required in sections where, under thecharacteristic combination of loads and the characteristic value of prestress, the concrete iscompressedortheabsolutevalueofthetensilestressintheconcreteisbelow fct,eff .
Table 13.4Ratio of bond strength, j , between tendons and reinforcing steel
Prestressing steel j
Pre-tensioned Bonded, post-tensioned
≤ C50/60 ≥ C70/85
Smooth bars and wires Notapplicable 0.3 0.15
Strands 0.6 0.5 0.25
Indented wires 0.7 0.6 0.30
Ribbed bars 0.8 0.7 0.35
NoteForintermediatevaluesbetweenC50/60andC70/85interpolationmaybeused.
BS EN 1992-1-1 Fig 7.1
BS EN 1992-1-1 7.3.2 (4)
BS EN 1992-1-1table 6.2
83
Serviceability
Control of deflection
The calculation method adopted shall represent the true behaviour of the structure underrelevantactionstoanaccuracyappropriatetotheobjectivesofthecalculation.
Memberswhicharenotexpectedtobeloadedabovethelevelwhichwouldcausethetensilestrengthoftheconcretetobeexceededanywherewithinthemembershouldbeconsideredtobeuncracked.Memberswhichareexpectedtocrack,butmaynotbefullycracked,willbehaveinamannerintermediatebetweentheuncrackedandfullycrackedconditionsand,formemberssubjected mainly to flexure, an adequate prediction of behaviour is given in the followingexpression:
a = z aII + (1 – z) aI
where a = deformationparameterconsideredwhichmaybe,forexample,astrain,a
curvature,orarotation.(Asasimplification,amayalsobetakenasadeflection–seebelow)
aI, aII = thevaluesoftheparametercalculatedfortheuncrackedandfullycrackedconditionsrespectively
z = distributioncoefficient(allowingfortensioningstiffeningatasection) = 1– b(ssr /ss)2
= 0foruncrackedsections b = coefficienttakingaccountoftheinfluenceofthedurationoftheloadingorof
repeatedloadingontheaveragestrain = 1.0forasingleshort-termloading = 0.5forsustainedloadsormanycyclesofrepeatedloading ss = stressinthetensionreinforcementcalculatedonthebasisofacrackedsection ssr = stressinthetensionreinforcementcalculatedonthebasisofacrackedsection
undertheloadingconditionscausingfirstcracking
Note:ssr /ssmaybereplacedbyMcr/MforflexureorNcr/Nforpuretension,whereMcristhecrackingmomentandNcristhecrackingforce.
Deformations due to loading may be assessed using the tensile strength and the effectivemodulusofelasticityoftheconcrete.
Table3.1indicatestherangeoflikelyvaluesfortensilestrength.Ingeneral,thebestestimateofthe behaviour will be obtained if fctm is used.Where it can be shown that there are no axialtensilestresses(e.g.thosecausedbyshrinkageorthermaleffects)theflexuraltensilestrength,fctm,fl,maybeused.
fctm,fl = MAX{(1.6– h/1000)fctm;fctm }
where h = totalmemberdepthinmm fctm = meanaxialtensilestrengthfromTable3.1
Forloadswithadurationcausingcreep,thetotaldeformationincludingcreepmaybecalculatedbyusinganeffectivemodulusofelasticityforconcreteaccordingtothefollowingExpression
Ec,eff = Ecm / (1 + h (∞,t0))
where h (∞,t0)=creepcoefficientrelevantfortheloadandtimeinterval(seeSection3.1.2)
Shrinkagecurvaturesmaybeassessedfromthefollowing:
1/rcs=easaeS/I
where 1/rcs = curvatureduetoshrinkage
13.6
BS EN 1992-1-1 7.4.3(2)
BS EN 1992-1-1 7.4.3(3)
BS EN 1992-1-1Exp. (7.18)
BS EN 1992-1-1 7.4.3(4)
BS EN 1992-1-1 3.1.8
BS EN 1992-1-1 7.4.3(5)
BS EN 1992-1-1 7.4.3(6)
84
ecs = freeshrinkagestrain(seeSection3.1.3) S = firstmomentofareaofthereinforcementaboutthecentroidofthesection I = secondmomentofareaofthesection ae = effectivemodularratio = Es/Ec,eff
Sand Ishouldbecalculatedfortheuncrackedconditionandthefullycrackedcondition,thefinalcurvaturebeingassessedusingtheExpressionforaabove.
Themostrigorousmethodofassessingdeflectionsusingthemethodgivenaboveistocomputethe curvatures at frequent sections along the member and then calculate the deflection bynumerical integration. In most cases it will be acceptable to compute the deflection twice,assumingthewholemembertobe in theuncrackedandfullycrackedcondition inturn,andtheninterpolateusingtheExpressionforaabove.
BS EN 1992-1-1 7.4.3(7)
85
Detailing–generalrequirements
Detailing – general requirementsGeneral
The rules given in this section apply to ribbed reinforcement, welded mesh and prestressingtendonsusedinstructuressubjectpredominantlytostaticloading.
Unlessotherwisestated,therulesforindividualbarsalsoapplyforbundlesofbarsforwhichanequivalentdiameterfn=f(nb)0.5shouldbeusedinthecalculations.InthisExpression,nbisthenumberofbarsinthebundle.Avaluefornbshouldbelimitedtofourverticalbarsincompressionandinlappedjoints,andtothreeinallothercases.Thevalueoffnshouldbelessthanorequalto55mm.
Thecleardistancebetween(andthecoverto)bundledbarsshouldbemeasuredfromtheactualexternalcontourofthebundledbars.Barsareallowedtotouchoneanotheratlapsandtheyneednotbetreatedasbundledbarsundertheseconditions.
Spacing of bars
Thespacingofbarsshouldbesuchthatconcretecanbeplacedandcompactedsatisfactorilyforthedevelopmentofbond.
Thecleardistancebetweenindividualparallelbarsorbetweenhorizontallayersofparallelbarsshouldnotbelessthanthe bardiameter, theaggregatesize+ 5mm, or20mm,whicheveristhegreatest.
Wherebarsarepositionedinseparatehorizontallayers,thebarsineachlayershouldbelocatedverticallyaboveeachother.Thereshouldbesufficientspacebetweentheresultingcolumnsofbarstoallowaccessforvibratorstogivegoodcompactionoftheconcrete.
Mandrel sizes for bent bars
Thediametertowhichabarisbentshouldbesuchastoavoiddamagetothereinforcementandcrushingofconcreteinsidethebendofthebar.Toavoiddamagetoreinforcementthemandrelsizeisasfollows: 4f, forbardiameterf≤16mm 7f, forbardiameterf>16mm 20f, formeshbentafterweldingwheretransversebarisonorwithin4fofthebend.
Otherwise 4f, or 7f, asabove.WeldingmustcomplywithISO/FDIS17660-2[22].
Themandreldiameterfmtoavoidcrushingofconcreteinsidethebendneednotbecheckedif:Anchorageofthebardoesnotrequirealengthmorethan5■■ fpasttheendofthebend;andThebarisnotpositionedatanedgeandthereisacrossbar(ofdiameter≥■■ f)insidethebend,andDiametersnotedaboveareused.■■
Otherwisethefollowingminimummandreldiameterfm,minshouldbeused:
fm,min≥Fbt((1/ab)+1/(2f))/fcd
where Fbt = tensileforceinthebaratthestartofthebendcausedbyultimateloads ab = halfthecentretocentrespacingofbars(perpendiculartotheplaneofthe
bend).Forbarsadjacenttothefaceofthemember,ab=cover+0.5f fcd = 0.85 fck/ 1.5
ThevalueoffcdshouldnotbetakengreaterthanthatforconcreteclassC55/67
where fck = characteristiccylinderstrength
14 14.1
14.2
14.3
BS EN 1992-1-1 8.1(1)
BS EN 1992-1-1 8.9.1(1) & (2)
BS EN 1992-1-1 8.9.1(3) & (4)
BS EN 1992-1-1 8.2
BS EN 1992-1-1 8.3(1) & (2)
BS EN 1992-1-1 table 8.1N & NA
BS EN 1992-1-1 8.3(3)
BS EN 1992-1-1 Exp. (8.1)
BS EN 1992-1-13.1.6(1) & NA to BS EN 1992-2
86
Anchorage of bars
General
Allreinforcementshouldbesoanchoredthattheforcesinthemaresafelytransmittedtothesurroundingconcretebybondwithoutcausingcracksorspalling.ThecommonmethodsofanchorageoflongitudinalbarsandlinksareshowninFigures14.1and14.2.
a) Basic anchorage length lb,rqd, for any shape measured along the centreline
lb,rqd
f
lbd
b) Equivalent anchorage length for standard bend 90º a < 150º where lb,eq = a1 lb,rqd
lb,eq
≥5f
a
e) Welded transverse bar where lb,eq = a4 lb,rqd
lb,eq
≥5ff≥0.6f
c) Equivalent anchorage length for standard hook where lb,eq = a1 lb,rqd
lb,eq
≥150º
≥5f
d) Equivalent anchorage length for standard loop where lb,eq = a1 lb,rqd
lb,eq
Keylbd = designanchoragelengthlb,req = basicanchoragelengthlb,eq = equivalentanchoragelength
Figure 14.1Methods of anchorage other than by a straight bar
c) Two welded transverse bars
d) Single welded transverse bar
f f f f
5f,but≥50mm
10f,but≥70mm
≥0.7f
≥2f ≥1.4f≥10mm
≥10mm
≥20mm
≤50mm
Figure 14.2Anchorage of links
14.4
14.4.1
BS EN 1992-1-1 8.4(1) & (2)
BS EN 1992-1-1 fig. 8.1
BS EN 1992-1-1 fig. 8.5
87
Detailing–generalrequirements
Design anchorage length lbd
Thedesignanchoragelengthlbdis
lbd =(a1a2a3a4a5)lb,rqd≥lb,min
where a1 = factordealingwiththeformofbarassumingadequatecover
=0.7forbentbarsintensionwherecd>3f,wherecdisdefinedinFigure14.3=1.0otherwiseforbarsintension=1.0forbarsincompression
a2 = factordealingwitheffectofconcreteminimumcover
=1–0.15(cd–f)/f≥0.7forstraightbarsintensionbut≤1.0=1–0.15(cd–3f)/f≥0.7forbentbarsintensionbut≤1.0=1.0otherwiseforbarsintension=1.0forbarsincompression
a3 = factordealingwitheffectofconfinementbytransversereinforcement
=1.0generally
a4 = factordealingwiththeeffectofinfluenceofweldedtransversebars
=0.7foraweldedtransversebarconformingwithFigure14.1e)=1.0otherwise
a5 = factordealingwiththeeffectofpressuretransversetotheplaneofsplittingalongthedesignanchoragelength
=1.0generally
lb,rqd = basicanchoragelength(seeSection14.4.3) lb,min = theminimumanchoragelength ≥ MAX{0.3lb,rqd;10f;100mm}intensionbars;and ≥ MAX{0.6lb,rqd;10f;100mm}incompressionbars.
Theproduct(a2a3a5)≥ 0.7
Figure 14.3Values of
cd for beams and slabs
a) Straight bars cd = minimum of a/2, c or c1
b) Bent or hooked bars cd = minimum of a/2 or c1
c1
c1
c
a a
Note
candc1aretakentobenominalcovers
Basic anchorage length lb,rqd
lb,rqd = basicanchoragelengthrequired=(f/4)(ssd/fbd)
where f = diameterofthebar ssd= designstressinthebaratthepositionfromwheretheanchorageismeasured fbd = ultimatebondstress(seeSection14.5)
Theanchoragelengthshouldbemeasuredalongthecentrelineofthebarinbentbars.
14.4.2
14.4.3
BS EN 1992-1-1 8.4.4(1) & table 8.2
BS EN 1992-1-1 fig. 8.3
BS EN 1992-1-1 8.4.3
88
Equivalent anchorage length lb,eq
Asasimplification
FortheshapesshowninFigure14.1b)tod)anequivalentanchoragelength■■ lb,eqmaybeusedwherelb,eq=a1lb,rqd.
ForthearrangementshowninFigure14.1e)■■ lb,eq=a4lb,req.
Ultimate bond stress
Theultimatebondstress,fbd,forribbedbarsmaybetakenas(seealsoTable14.1)
fbd=2.25n1n2fctd
where n1 = coefficientrelatedtothequalityofthebondconditionandthepositionofthebar
duringconcreting = 1.0for‘good’bondconditions(seeFigure14.4fordefinition) = 0.7forallothercasesandforbarsinstructuralelementsbuiltusingslipforms n2 = coefficientrelatedtobardiameter = 1.0forbardiameter≤32mm = (132–f)/100forbardiameter>32mm fctd = (actfctk,0.05/gC)isthedesignvalueoftensilestrengthusingthevalueoffctk,0.05
obtainedfromTable3.1,act= 1.0 andgC= 1.5. Duetothebrittlenessofhigherstrengthconcretefctk,0.05shouldbelimitedheretothevalueforC60/75,unlessitcanbeverifiedthattheaveragebondstrengthincreasesabovethislimit
Directionofconcreting Directionofconcreting
Directionofconcreting
Directionofconcreting
Key
b) h 250 mm d) h > 600 mm
hh
300
c) h > 250 mm
250
a) 45º a 90º
a
‘good’bondconditions
‘poor’bondconditions
Figure 14.4Description of bond conditions
14.4.4
14.5
BS EN 1992-1-1 8.4.4(2)
BS EN 1992-1-1 8.4.2(2)
BS EN 1992-2 3.1.6(102) & NA
BS EN 1992-1-1 fig. 8.2
89
Detailing–generalrequirements
Table 14.1 Design bond stress for different bond conditions
Design bond stress f bd (N/mm2)
C25/30 C30/37 C35/45 C40/50 C45/55 C50/60 C55/67 C60/75
Good bond & f ≤ 32 mm
2.7 3.0 3.3 3.8 4.1 4.4 4.5 4.7
Good bond & f = 40 mm
2.5 2.8 3.0 3.5 3.7 4.0 4.1 4.3
Poor bond & f ≤ 32 mm
1.9 2.1 2.3 2.6 2.8 3.0 3.2 3.3
Poor bond & f = 40 mm
1.7 1.9 2.1 2.4 2.6 2.8 2.9 3.0
Anchorage of tendons at ULS
The anchorage of tendons should be checked in sections where the concrete tensile stressexceeds fctk,0.05 ( fctk,0.05 should not exceed the value for class C60/75 concrete). The total
anchoragelengthforatendonwithastressspdis:
lbpd=lpt2+(a2f(spd–spm,∞)/fbpd)
where lpt2=1.2(a1a2fspm,0/fbpt)
where a1 = 1.0forgradualreleaseofprestressand1.25forsuddenrelease spm,0 = stressinthetendonjustafterrelease fbpt = np1n1fctd(t) np1 = 2.7forindentedwiresand3.2for3-and7-wirestrands n1 = 1.0forgoodbondconditionsand0.7otherwise fctd(t) = designtensilevalueofstrengthatthetimeofrelease = 1.0 0.7fctm(t)/ 1.5
fctm(t) = (bcc(t))afctm
bcc(t) = coefficientwhichdependsontheageofloading
=exp {s[1–( 0.5]}28t
)
s = coefficientwhichdependsontypeofcement(seeSection3.1.2) = 0.20forcementstrengthclassesCEM42.5R,CEM52.5NandCEM52.5R(ClassR) = 0.25forcementstrengthclassesCEM32.5R,CEM42.5N(ClassN) = 0.38forcementstrengthclassCEM32.5(ClassS) t = ageofconcreteindays fctm = meanvalueofaxialtensilestrengthofconcrete(seeTable3.1) a =1fort <28 =2/3fort ≥28 a2 = 0.25forcirculartendonsand0.19for3-and7-wirestrands f = nominaldiameterofthetendon spd = tendonstresscorrespondingtotheforcecalculatedforacrackedsection spm,∞ = prestressafteralllosses fbpd = np2n1fctd,wherenp2=1.4forindentedwiresand1.2for7-wirestrands.
n1isdescribedinSection14.5
14.6
BS EN 1992-1-1 8.10.2.3
BS EN 1992-1-1 Exp. (8.21)
90
Anchorage of tendons at transfer of prestress
Thebasicvalueofthetransmissionlengthatthereleaseoftendons,lpt,isgivenby:
lpt=a1a2fspm,0/fbpt
where a1 = 1.0forgradualrelease = 1.25forsuddenrelease a2 = 0.25fortendonswithcircularcross-section = 0.19for3-and7-wirestrands f = nominaldiameteroftendon spm,0 = tendonstressjustafterrelease fbpt = bondstress = np1n1fctd(t)
where np1 = coefficientthattakesintoaccountthetypeoftendonandthebond
situationatrelease = 2.7forindentedwires = 3.2for3-and7-wirestrands n1 =1.0forgoodbondconditions = 0.7otherwise,unlessahighervaluecanbejustifiedwithregardtospecial
circumstancesinexecution fctd(t) = designtensilevalueofstrengthattimeofrelease(seeSection14.6)
Thedesignvalueofthetransmissionlengthshouldbetakenasthelessfavourableoftwovalues,dependingonthedesignsituation:
lpt1 =0.8lpt
orlpt2=1.2lptNormallythelowervalueisusedforverificationsoflocalstressesatrelease,thehighervalueforultimatelimitstates(shear,anchorageetc.).
Laps
General
Forces are transmitted from one bar to another by lapping, welding or using mechanicaldevices.
Lapsbetweenbarsshouldnormallybestaggeredandnot located inareasofhighmoments/forces.Allbarsincompressionandsecondaryreinforcementmaybelappedatoneplace.
Lapping bars
LapsofbarsshouldbearrangedasshowninFigure14.5.
Thedesignlaplengthl0is:
l0=a1a2a3a4a5a6lb,rqd≥l0,min
where a6 = (r1/25)0.5.1<a6<1.5(seeTable14.2) r1 = percentageofreinforcementlappedwithin0.65l0fromthecentre lineofthelap
beingconsidered l0,min≥ MAX{0.3a6lb,rqd;15h;200mm}
a1,a2,a3,a4anda5aredescribedinSection14.4.2
14.7
14.8
14.8.1
14.8.2
BS EN 1992-1-1 8.7
BS EN 1992-1-1 8.7.2(2) & 8.7.3
BS EN 1992-1-1 Exp. (8.10)
BS EN 1992-1-1 8.10.2.2(2)
BS EN 1992-1-1 Exp. (8.16)
91
Detailing–generalrequirements
Table 14.2Values of coefficient a6
r1, % lapped bars relative to total cross-sectional area
< 25% 33% 50% > 50%
a6 1.0 1.15 1.4 1.5
Fs
Fs
Fs
Fs
Fs
Fs
l0≥0.3l0
f
a
≤50mm
≥20mm
≤4f
≥2f
Figure 14.5Arranging adjacent lapping bars
Lapping fabric
LapsoffabricshouldbearrangedasshowninFigure14.6.
Whenfabricreinforcementislappedbylayering,thefollowingshouldbenoted:
Calculatedstressinthelappedreinforcementshouldnotbemorethan80%ofthe■■
designstrength;ifnot,themomentofresistanceshouldbebasedontheeffectivedepthtothelayerfurthestfromthetensionfaceandthecalculatedsteelstressshouldbeincreasedby25%forthepurposesofcrackcontrol.Permissiblepercentageoffabricmainreinforcementthatmaybelappedinanysectionis:■■
100%if(As/s)≤1200mm2/m(wheresisthespacingofbars)60%ifAs/s>1200mm2/m.Allsecondaryreinforcementmaybelappedatthesamelocationandtheminimumlap■■
lengthl0,minforlayeredfabricisasfollows:
≥150mmforf≤6mm≥250mmfor6mm<f<8.5mm≥350mmfor8.5mm<f<12mm
Thereshouldgenerallybeatleasttwobarpitcheswithinthelaplength.Thiscouldbereducedtoonebarpitchforf≤6mm.
Figure 14.6Lapping of
welded fabric
a) Intermeshed fabric (longitudinal section)
b) Layered fabric (longitudinal section)
Fs
Fs
Fs
Fs
l0
l0
14.8.3BS EN 1992-1-1 8.7.5
BS EN 1992-1-1 fig. 8.10
BS EN 1992-1-1 8.7.5.1(7)8.7.5.2(1)
BS EN 1992-1-1 fig. 8.7
92
14.8.4
14.8.5
Transverse reinforcement
Transversereinforcementisrequiredinthelapzonetoresisttransversetensionforces.
Wherethediameterofthelappedbarislessthan20mmorthepercentageofreinforcementlappedatanysectionislessthan25%,thenanytransversereinforcementorlinksnecessaryforother purposes may be deemed sufficient for the transverse tensile forces without furtherjustification.
Whentheaboveconditionsdonotapply,transversereinforcementshouldbeprovidedasshowninFigure14.7.Wheremorethan50%ofbarsarelappedatonesectionandthespacingbetweenadjacentlaps(dimensionainFigure14.5)<10f,thetransversereinforcementshouldbeintheformoflinksorUbarsanchoredintothebodyofthesection.
InFigure14.7,thetotalareaoftransversereinforcementatlapsSAst>Asofonelappedbar.
Figure 14.7Transverse
reinforcement for lapped splices
a) Bars in tension
b) Bars in compression
Fs
Fs
FsFs
l0
l0
l0/3 l0/3
l0/3 l0/3
SAst/2 SAst/2
SAst/2 SAst/2
4f 4f
≤150mm
≤150mm
Lapping large bars
Forbarslargerthan 40mm indiameterthefollowingadditionalrequirementsapply:
Barsshouldbeanchoredusingmechanicaldevices.Asanalternativetheymaybeanchored■■
asstraightbars,butlinksshouldbeprovidedasconfiningreinforcement.■■■ Barsshouldnotbelappedexceptinsectionswithaminimumdimensionof1morwherethestressisnotgreaterthan80%oftheultimatestrength.
Intheabsenceoftransversecompression,transversereinforcement,inadditiontothat■■
requiredforotherpurposes,shouldbeprovidedintheanchoragezoneatspacingnotexceeding5timesthediameterofthelongitudinalbar.ThearrangementshouldcomplywithFigure14.8.
BS EN 1992-1-1 fig. 8.9
BS EN 1992-1-1 8.8
BS EN 1992-1-1 8.7.4
93
Detailing–generalrequirements
BS EN 1992-1-1 fig. 8.11
Figure 14.8Additional
reinforcement in an anchorage for
large diameter bars where there
is no transverse compression
Anchoredbar Continuingbar
a) n1 = 1, n2 = 2 b) n1 = 2, n2 = 2
SAsh≥0.5As1SAsh≥0.25As1
SAsv≥0.5As1 SAsv≥0.5As1
As1 As1
Note
n1=numberoflayers,n2=numberofbars
94
15 15.1
15.2
15.2.1
Detailing – particular requirementsGeneral
Thissectiongivesparticular requirements fordetailingofstructuralelements.Theseare inadditiontothoseoutlinedinSections13and14.
Beams
Longitudinal bars
TheareaoflongitudinalreinforcementshallnotbetakenaslessthanAs,min
As,min=0.26(fctm/fyk)btd≥0.0013btd
where fctm = meanaxialtensilestrengthofconcrete(seeTable3.1) fyk = characteristicyieldstrengthofreinforcement bt = meanwidthofthetensionzone;foraT-beamwiththeflangeincompression,only
thewidthofthewebistakenintoaccountincalculatingthevaluebt d = effectivedepthValuesofAs,minforvariousstrengthclassesareprovidedinTable15.1
Thecross-sectionalareaoftensionorcompressionreinforcementis 0.04Ac outsidelaplocations.
Any compression longitudinal reinforcement which is included in the resistance calculationshouldbeheldbytransversereinforcementwithspacingnotgreaterthan15timesthediameterofthelongitudinalbar.
Wherethedesignofasectionhasincludedthecontributionofanylongitudinalcompressionreinforcement in the resistance calculation, such longitudinal compression reinforcementshould be effectively restrained by transverse reinforcement. Effective restraint may beachievedbysatisfyingallofthefollowingconditions.
Linksshouldbesoarrangedthateverycornerandalternatebarorgroupinanouter■■
layerofcompressionreinforcementisheldinplacebyalinkanchoredinaccordancewithFigure14.2a)orb).Allothercompressionreinforcementshouldbewithin150mmofabarheldinplaceby■■
alink.Theminimumsizeofthetransversereinforcementandlinks,wherenecessary,shouldbe■■
notlessthan6mmoronequarterofthediameterofthelongitudinalbars,whicheverisgreater.
Table 15.1Minimum area of longitudinal reinforcement as a proportion of btd
Strength class
C25/30 C28/35 C30/37 C32/40 C35/45 C40/50 C45/55 C50/60 C55/67 C60/75 C70/85
As,min as a % of btd
0.13 0.14 0.15 0.16 0.17 0.18 0.20 0.21 0.22 0.23 0.24
For members prestressed with permanently unbonded tendons or with external prestressingcables,itshouldbeverifiedthattheultimatebendingcapacityislargerthantheflexuralcrackingmoment.Acapacityof1.15timesthecrackingmomentissufficient.
BS EN 1992-1-1 9.1
BS EN 1992-1-1 9.2.1.1
BS EN 1992-1-1 9.2.1.2(3)
PD 6687-210.2
BS EN 1992-1-1 9.2.1.1(4)
95
Detailing–particularrequirements
Curtailment
Sufficientreinforcementshouldbeprovidedatallsectionstoresisttheenvelopeoftheactingtensileforce.Theresistanceofbarswithintheiranchoragelengthsmaybetakenintoaccountassuminglinearvariationofforce.
Thelongitudinaltensileforcesinthebarsincludethosearisingfrombendingmomentsandthosefromthetrussmodelforshear.AsmaybeseenfromFigure15.1,thoseforcesfromthetrussmodelforshearmaybeaccommodatedbydisplacingthelocationwhereabarisnolongerrequiredforbendingmomentbyadistanceofalwhere
al=z(coty–cota)/2
where y = strutangleusedforshearcalculations(seeFigure7.3) a = angleoftheshearreinforcementtothelongitudinalaxis(seeFigure7.3)
Forallbuthighshearcoty=2.5;forverticallinkscota=0;sogenerallyal=1.25z.
Hoggingreinforcement
EnvelopeofMEd/z +NEd
ActingtensileforceFs
ResistingtensileforceFRs
Saggingreinforcement
lbd
lbd
lbd
lbd
lbd
lbd
lbd
lbd
al
al
DFtd
DFtd
Figure 15.1Illustration of the curtailment of longitudinal reinforcement, taking into account the effect of inclined cracks and the resistance of reinforcement within anchorage lengths
Top reinforcement in end supports
In monolithic construction, (even when simple supports have been assumed in design) thesectionatsupportsshouldbedesignedforbendingmomentarisingfrompartialfixityofatleast25%ofthemaximumbendingdesignmomentinspan.
15.2.2
15.2.3
BS EN 1992-1-1fig. 9.2
BS EN 1992-1-1 9.2.1.3
BS EN 1992-1-19.2.1.2(1) & NA
96
Bottom reinforcement in end supports
Theareaofbottomreinforcementprovidedatendswithlittleornofixityassumedinthedesignshould be at least 25% of the area of the steel provided in the span.The bars should beanchoredtoresistaforce,FEd,of
FEd=( |VEd| al /z)+NEd
where
|VEd|= absolutedesignvalueofshearforce NEd = axialforce, al,isasdefinedinSection15.2.2
Theanchorageismeasuredfromthelineofcontactbetweenthebeamandthesupport.
Intermediate supports
Atintermediatesupportsofcontinuousbeams,thetotalareaoftensionreinforcement,As,ofaflanged cross-section should be spread over the effective width of the flange (as defined inFigure15.2).Partofitmaybeconcentratedoverthewebwidth.
beff
beff1 beff2
As
bw
hf
Figure 15.2Placing of tension reinforcement in flanged cross-section
Shear reinforcement
Whereacombinationoflinksandbentupbarsisusedasshearreinforcement,atleast50%ofthereinforcementrequiredshouldbeintheformoflinks.Thelongitudinalspacingofshearassemblies should not exceed 0.75d(1+cota) , and spacing of bent-up bars should notexceed 0.6d(1+cota) where a is the inclination of the shear reinforcement to thelongitudinalaxisofthebeam.Thetransversespacingofthelegsofshearlinksshouldnotexceed0.75d≤600mm .
A minimum area of shear reinforcement should be provided to satisfy the followingExpression:
Asw/(s bwsina)≥0.08fck0.5/fyk
where s = longitudinalspacingoftheshearreinforcement bw= breadthofthewebmember a = angleoftheshearreinforcementtothelongitudinalaxisofthemember. Forverticallinkssina=1.0.
15.2.4
15.2.5
15.2.6
BS EN 1992-1-1 9.2.1.2(2)
BS EN 1992-1-1 fig. 9.1
BS EN 1992-1-1 9.2.2(4),(6)&(7)
BS EN 1992-1-1 9.2.2(5) & NA
97
Detailing–particularrequirements
15.2.7
15.2.8
Torsion reinforcement
Wherelinksarerequiredfortorsion,theyshouldcomplywiththeanchorageshowninFigure15.3.Themaximumlongitudinalspacingofthetorsionlinkssl,maxshouldbe:
sl,max≤MIN{u/8;0.75d(1+cota);h;b}
where u = circumferenceofouteredgeofeffectivecross-section(seeFigure9.1) d = effectivedepthofbeam h = heightofbeam b = breadthofbeam
Thelongitudinalbarsrequiredfortorsionshouldbearrangedsuchthatthereisatleastonebarateachcornerwiththeothersbeingdistributeduniformlyaroundthe innerperipheryofthelinksataspacingnotexceeding350mm.
a1) a2) a3)
a) Recommended shapes b) Shape not recommendedNoteThesecondalternativefora2)shouldhaveafulllaplengthalongthetop
or
Figure 15.3Examples of shapes for torsion links
Indirect supports
Whereabeamissupportedbyabeam,insteadofawallorcolumn,reinforcementshouldbeprovided to resist the mutual reaction.This reinforcement is in addition to that required forother reasons. The supporting reinforcement between two beams should consist of linkssurroundingtheprincipalreinforcementofthesupportingmember.Someoftheselinksmaybedistributedoutsidethevolumeofconcretecommontothetwobeams.SeeFigure15.4.
Figure 15.4Plan section
showing supporting
reinforcement in the intersection
zone of two beams
Supportedbeamwithheighth2(h1≥h2)
Supportingbeamwithheighth1
≤h2/3
≤h2/2
≤h1/3
≤h1/2
BS EN 1992-1-1fig. 9.6
BS EN 1992-1-19.25
BS EN 1992-1-1fig. 9.7
BS EN 1992-1-1 9.2.3
98
15.3
15.3.1
15.3.2
15.3.3
15.3.4
15.4
15.4.1
15.4.2
One-way and two-way spanning slabs
Main (principal) reinforcement
TheminimumandmaximumsteelpercentagesinthemaindirectioninSection15.2.1apply.
The spacing of main reinforcement should not exceed 3h (but not greater than 400mm),wherehisthetotaldepthoftheslab.Inareaswithconcentratedloadsorareasofmaximummomenttheseprovisionsbecomerespectively 2hand ≤250mm .
Secondary (distribution) reinforcement
Secondary reinforcement of not less than 20% of the principal reinforcement should beprovidedinone-wayslabs.
The spacing of secondary reinforcement should not exceed 3.5h (but not greater than450mm).Inareaswithconcentratedloads,orinareasofmaximummoment,theseprovisions
becomerespectively 3h(butnotgreaterthan 400mm).
Reinforcement in slabs near supports
In simply supported slabs, half the calculated span reinforcement should continue up to thesupportandbeanchoredthereininaccordancewithSection14.4.2.
Wherepartialfixityoccursalonganedgeofaslabbutisnottakenintoaccountintheanalysis,thetopreinforcementshouldbecapableofresistingatleast25%ofthemaximummomentinthe adjacent span. This reinforcement should extend at least 0.2 times the length of theadjacentspanmeasuredfromthefaceofthesupport.Atanendsupportthemomenttoberesistedmaybereducedto15%ofthemaximummomentintheadjacentspan.
Shear reinforcement
Aslabinwhichshearreinforcementisprovidedshouldhaveadepthofatleast200mm.
Whereshearreinforcementisprovidedtherulesforbeamsmaybefollowed.
Flat slabs
Details at internal columns
Atinternalcolumns,unlessrigorousserviceabilitycalculationsarecarriedout,topreinforcementwithanareaof0.5Atshouldbeplacedoverthecolumninawidthequaltothesumof0.125times the panel width on either side of the column. At represents the area of reinforcementrequiredtoresistfullnegativemomentfromthesumofthetwohalfpanelsoneachsideofthecolumn. Bottom bars (≥ 2 bars) in each orthogonal direction should be provided at internalcolumnsandthisreinforcementshouldpassthroughthecolumn.
Details at edge and corner columns
ReinforcementperpendiculartoafreeedgerequiredtotransmitbendingmomentsfromtheslabtoanedgeorcornercolumnshouldbeplacedwithintheeffectivewidthbeshowninFigure15.5.
BS EN 1992-1-19.3
BS EN 1992-1-19.3.1.1(1)
BS EN 1992-1-19.3.1.1(3) & NA
BS EN 1992-1-19.3.1.1(3) & NA
BS EN 1992-1-1 9.3.1.2
BS EN 1992-1-1 9.3.2
99
Detailing–particularrequirements
15.4.3
a) Edge column b) Corner column
Noteyisthedistancefromtheedgeoftheslabtotheinnermostfaceofthecolumn
Slabedge
Slabedge
Slabedge
ycanbe>cy zcanbe>cxandycanbe>cy
be=cx+ybe=z+y/2
cycy
cxcx
y
y
z
Figure 15.5Effective width, be, of a flat slab
Punching shear reinforcement
Wherepunchingshearreinforcementisrequired,itshouldbeplacedbetweentheloadedarea /columnand 1.5dinsidethecontrolperimeteratwhichreinforcementisnolongerrequired.
The spacing of link legs around a perimeter should not exceed 1.5d within the first controlperimeter(2dfromtheloadedarea)andshouldnotexceed2dforperimetersoutsidethefirstcontrolperimeter(seeFigure15.6).
Outerperimeterofshearreinforcement
Outercontrolperimeteruout
≤1.5d a1.5d
0.5d
≤0.75d
st
sr
A A
Notes1ForsectionA–A
refertoFigure15.72Nationalvalueshavebeenused
Keya≤2.0dif>2d
fromcolumn
Figure 15.6Layout of flat slab shear reinforcement
BS EN 1992-1-1fig. 9.9
BS EN 1992-1-1 9.4.1(2) & (3)
BS EN 1992-1-1 9.4.2(1)
BS EN 1992-1-1 9.4.3
100
BS EN 1992-1-19.5.3(1) & NA
BS EN 1992-1-1 9.4.3(2)
BS EN 1992-1-1 9.5.2 & NA
15.5
15.5.1
15.5.2
Outercontrolperimeterrequiringshearreinforcement
Outercontrolperimeternotrequiringshearreinforcement,uout
≤1.5d
>0.3d≤0.5d
sr≤0.75d
Figure 15.7Section A – A from Figure 15.6: spacing of punching shear reinforcing links
Theintentionistoprovideanevendistribution/densityofpunchingshearreinforcementwithinthezonewhereitisrequired(seeSection8.8).
Thecontrolperimeteratwhichshearreinforcementisnotrequired,Uout,shouldbecalculatedfromthefollowingExpression:Uout=bVEd/(VRd,cd)
Theoutermostperimeterofshearreinforcementshouldbeplacednotgreaterthan1.5dwithinUout.
Whereshearreinforcementisrequired,theareaofalinkleg,Asw,minisgivenbythefollowingExpression:
Asw,min(1.5sina+cosa)/(srst)≥0.08fck0.5/fyk
where srandst = spacing of shear reinforcement in radial and tangential directions respectively
(seeFigure15.6)
Columns
Longitudinal reinforcement
Longitudinalbarsshouldhaveadiameterofnotlessthan 12mm.
ThetotalamountoflongitudinalreinforcementshouldnotbelessthanAs,min:
As,min≥MAX{0.1NEd/fyd;0.002Ac}
where NEd= designaxialcompressionforce fyd = designyieldstrengthofthereinforcement Ac = cross-sectionalareaofconcrete
The area of longitudinal reinforcement should not exceed 0.04Acoutside lap locations.Thislimitshouldbeincreasedto0.08Acatlaps.
Transverse reinforcement (links)
Thediameterofthetransversereinforcement(links,loopsorhelicalspiralreinforcement)shouldnotbelessthan6mmoronequarterofthediameterofthelongitudinalbars,whicheverisgreater.
BS EN 1992-1-1 6.4.5(4) & NA
BS EN 1992-1-1 fig. 9.10
101
Detailing–particularrequirements
15.6
15.6.1
15.6.2
15.6.3
Thespacingofthetransversereinforcementalongthecolumnshouldnotexceed:
20timesthediameterofthelongitudinalbar,or■■
thelesserdimensionofthecolumn,or■■
400mm.■■
Themaximumspacingrequiredaboveshouldbereducedbyafactorof0.6:
Insectionswithinadistanceequaltothelargerdimensionofthecolumncross-section■■
aboveandbelowabeamorslab.Nearlappedjoints,ifthemaximumdiameterofthelongitudinalbarsisgreaterthan14mm.■■
Aminimumof3barsevenlyplacedinthelaplengthisrequired.
Wherethedirectionofthelongitudinalbarschanges,thespacingoftransversereinforcementshouldbecalculatedtakingintoaccountthetransverseforces involved.Theseeffectsmaybeignoredifthechangeofdirectionislessthanorequalto1in12.
Wherethedesignofasectionhasincludedthecontributionofanylongitudinalcompressionreinforcement in the resistance calculation, such longitudinal compression reinforcementshould be effectively restrained by transverse reinforcement. Effective restraint may beachievedbysatisfyingallofthefollowingconditions:
Linksshouldbesoarrangedthateverycornerandalternatebarorgroupinanouter■■
layerofcompressionreinforcementisheldinplacebyalinkanchoredinaccordancewithFigure14.2a)orb).
Allothercompressionreinforcementshouldbewithin150mmofabarheldinplaceby■■
alink.Theminimumsizeofthetransversereinforcementandlinks,wherenecessary,shouldbenot■■
lessthan6mmoronequarterofthediameterofthelongitudinalbars,whicheverisgreater.
For circular columns, where the longitudinal reinforcement is located round the peripheryadequatelateralsupportisprovidedbyacirculartiepassingroundthebarsorgroups.
Walls
Vertical reinforcement
The area of vertical reinforcement should lie between 0.002Ac and 0.04Ac outside lapslocations.Thislimitmaybedoubledatlaps.
Thedistancebetweentwoadjacentbarsshouldnotexceed3timesthewallthicknessor400mm,whicheveristhelesser.
Horizontal reinforcement
Horizontalreinforcementrunningparalleltothefacesofthewallshouldbeprovidedateachsurface. It should not be less than either 25% of the vertical reinforcement or 0.001Ac,whicheverisgreater.
Thespacingbetweentwoadjacenthorizontalbarsshouldnotbegreaterthan400mm.
Transverse reinforcement
Inanypartofawallwherethetotalareaofthevertical reinforcement inthetwofacesexceeds0.02Ac,transversereinforcementintheformoflinksshouldbeprovidedinaccordancewiththerulesforcolumns.
BS EN 1992-1-19.5.3(3) & (4)
BS EN 1992-1-19.5.3(5)
PD 6687-210.2
BS EN 1992-1-19.6.2 & NA
BS EN 1992-1-19.6.3 & NA
BS EN 1992-1-19.6.4
102
PD 6687-2 fig. 6
15.7
Where the main reinforcement is placed nearest to the wall faces, transverse reinforcementshould also be provided in the form of links with at least 4 per m2 of wall area.Transversereinforcementneednotbeprovidedwhereweldedmeshandbarsofdiameterf ≤16mmareusedwithconcretecoverlargerthan2f.
Pile caps
Thedistancefromtheouteredgeofthepiletotheedgeofthepilecapshouldbesuchthatthetieforcescanbeproperlyanchored.Theexpecteddeviationofthepileonsiteshouldbetakenintoaccount.
Reinforcement in a pile cap should be calculated either by using strut-and-tie or flexuralmethodsasappropriate.Themaintensilereinforcementtoresisttheactioneffectsshouldbeconcentrated in stress zones between the tops of the piles.The minimum diameter of barsshouldbe 12mm.
Wherethedistancebetweentheedgeofapileandapierislessthan2d,someoftheshearforceinthepilecapwillbetransmitteddirectlybetweenthepierandthepileviaastruttingaction.Thebasicpunchingperimetercannotbeconstructedwithoutencompassingapartofthesupportasshownforthe2dperimeterinFigure15.8.Insuchcases,itisrecommendedthatthetensionreinforcementisprovidedwithafullanchoragebeyondthelineofthepilecentres and that the shear design takes into consideration of the following in addition tootherverificationsrequiredbyBSEN1992-2:2005.
Flexural shear on plane passing across the full width of the pile cap■■ .Flexuralshearshouldbecheckedonplanespassingacrossthefullwidthofthepilecap,suchastheflexuralshearplaneinFigure15.8.Shearenhancementshouldbetakenintoaccountbyanincreasetotheconcreteresistanceandnotbyareductionintheshearforce.Wherethespacingofthepilecentresislessthanorequalto3pilediameters,theshortshearspanenhancementmaybeappliedoverthewholesection.Wherethespacingisgreaterthanthis,theenhancementmayonlybeappliedonstripsofwidth3pilediameterscentredoneachpile.Theshearspanavshouldbetakenasthedistancebetweenthefaceofthecolumnorwallandtheneareredgeofthepilesplus20%ofthepilediameter.
Maximum permissible shear stress for punching■■ .ThemaximumpermissibleshearstressatthefaceofthepilesandpiersshouldbecheckedinaccordancewithSection8.6.Theshearperimeterforcornerpilesshouldbethepileperimeter,oraperimeterpassingpartiallyaroundthepileandextendingouttothefreeedgesofthepilecap,whicheverisless.
Punching resistance of corner piles.■■ Cornerpilesshouldbecheckedforpunchingresistanceata2dperimeter(withoutsupportenhancement)ignoringthepresenceofthepierorsupportandanyverticalreinforcementwithinit.
FurtherguidanceisgiveninHendy&Smith[20].
Figure 15.8Corner piles
within 2d of a column base
2d perimeterFlexural shear plane across cap
BS EN 1992-2 9.8.1 (103) & NA
PD 6687-2 10.4
103
Detailing–particularrequirements
15.8
15.9
15.9.1
15.9.2
15.9.3
15.9.4
Bored piles
BoredpilesshouldhavetheminimumreinforcementshowninTable15.2. Aminimumofsixlongitudinalbarswithdiameterofatleast16mmshouldbeprovidedwithamaximumspacing of 200 mm around the periphery of the pile.The detailing should comply withBSEN1536[23].
Table 15.2Recommended minimum longitudinal reinforcement in cast-in-place bored piles
Area of cross-section of the pile (Ac) Ac ≤ 0.5 m2 0.5 m2 ≤ 1.0 m2 Ac > 1.0 m2
Minimum area of longitudinal reinforcement (As,bpmin)
≥0.005Ac ≥25cm2 ≥0.0025Ac
Requirements for voided slabs
PD6687-2givesthefollowingguidanceforthedesignofvoidedslabbridgedeckscastinsitu.
Transverse shear
Theeffectsofcelldistortionduetotransverseshearshouldbeconsidered.Inparticular:
Theincreasedstressesinthetransversereinforcementandshearlinksduetocell■■
distortionresultingfromtransverseshearshouldbecalculatedbyanappropriateanalysis(e.g.ananalysisbasedontheassumptionthatthetransverseactionactsinamannersimilartoaVierendeelframe).Theresistanceoftheflangesandwebstothelocalmomentsproducedbythetransverse■■
sheareffectsshouldbeverified.
Thetopandbottomflangesshouldbedesignedassolidslabs,eachtocarryapartoftheglobaltransverseshearforceproportionaltotheflangethickness.
Longitudinal shear
Thelongitudinalribsbetweenthevoidsshouldbedesignedasbeamstoresisttheshearforcesinthelongitudinaldirection,includinganyshearduetotorsionaleffects.
Punching
Punching of wheel loads through the top flange of decks with circular voids will generallyneedtobeconsideredforunusuallythinflanges,typicallythosewithvoiddiametertoslabdepthratiosofgreaterthan0.75.
Transverse reinforcement
Intheabsenceofadetailedanalysis,theminimumtransversereinforcementprovidedshouldbeasfollows:
Inthepredominantlytensileflangeeither1500mm■■ 2/mor1%oftheminimumflangesection,whicheveristhelesser.Inthepredominantlycompressiveflangeeither1000mm■■ 2/mor0.7%oftheminimumflangesection,whicheveristhelesser.
BS EN 1992-1-19.85
BS EN 1992-1-1table 9.6.N
PD 6687-210.5.2
PD 6687-210.5.3
PD 6687-210.5.4
PD 6687-210.5.5
104
BS EN 1992-1-1 fig. 8.14
BS EN 1992-1-1 fig. 8.15
BS EN 1992-1-1 8.10.1.3 (3)
PD 6687-29.2
15.10
15.10.1
15.10.2
The spacing of the transverse reinforcement should not exceed twice the minimumflangethickness.
Inskewvoidedslabs,itispreferableforthetransversesteeltobeplacedperpendiculartothevoidsandthelongitudinalsteeltobeplacedparalleltothevoids.
Prestressing
Arrangement of pre-tensioned tendons
Theminimumclearhorizontalandverticalspacingofindividualpre-tensionedtendonsshouldbeinaccordancewiththatshowninFigure15.9.
f≥dg
≥2f
≥dg+5
≥2f
≥20 mm
≥f≥40 mm
≥dg+5
≥f≥50 mm
≥dg
≥f≥40 mm
NoteWherefisthediameterofpre-tensionedtendonanddgisthemaximumsizeofaggregate
Figure 15.9Minimum clear spacing between pre-tensioned tendons
Arrangement of post-tensioned ducts
The minimum clear spacing of between ducts should be in accordance with that shown inFigure15.10.
Intheabsenceoftheprovisionofreinforcementbetweenductstopreventsplittingoftheconcrete,designedinaccordancewiththestrutandtierules(seeSection10),theminimumcentretocentreductspacingsshouldbeasgiveninTable15.3.ThesespacingsaregiveninBS5400-4:1990[24].
f≥dg
≥2f
≥dg+5
≥2f
≥20 mm
≥f≥40 mm
≥dg+5
≥f≥50 mm
≥dg
≥f≥40 mm
NoteWherefisthediameterofpost-tensionedductanddgisthemaximumsizeofaggregate
Figure 15.10Minimum clear spacing between post-tensioned ducts
BS EN 1992-1-1 8.10.1.2(1)
105
Detailing–particularrequirements
Table 15.3Minimum spacing of post-tensioning ducts (mm)
Radius of curvature of duct (m)
Duct internal diameter (mm)
19 30 40 50 60 70 80 90 100 110 120 130 140 150 160 170
Tendon force (kN)
296 387 960 1337 1920 2640 3360 4320 5183 6019 7200 8640 9424 10336 11248 13200
2 110 140 350 485 700 960
4 55 70 175 245 350 480 610 785 940 Radiinotnormallyused
6 38 60 120 165 235 320 410 525 630 730 870 1045
8 90 125 175 240 305 395 470 545 655 785 855 940
10 80 100 140 195 245 315 375 440 525 630 685 750 815
12 160 205 265 315 365 435 525 570 625 680 800
14 140 175 225 270 315 375 450 490 535 585 785
16 160 195 235 275 330 395 430 470 510 600
18 180 210 245 290 350 380 420 455 535
20 200 220 265 315 345 375 410 480
22 240 285 310 340 370 435
24 265 285 315 340 400
26 260 280 300 320 370
28 345
30 340
40 38 60 80 100 120 140 160 180 200 220 240 260 280 300 320 340
Notes
1Thetendonforceshownisthemaximumnormallyavailableforthegivensizeofduct(takenas80%ofthecharacteristicstrengthofthetendon).
2Valueslessthan2×ductinternaldiameterarenotincluded.
Connections
Connections transmitting compression
Connections without bedding material (dry connections) should only be used where anappropriate quality of workmanship can be achieved.The average bearing stress should notexceed0.3fcdwhere
fcd= 0.85fck/1.5
Intheabsenceofotherspecificationsthefollowingvaluecanbeusedforthebearingstrengthofotherconnections
fRd=fbed≤0.85fcd
where fcd = lowerofthedesignstrengthsforsupportedandsupportingmember
= 0.85fck/1.5
fbed= designstrengthofthebeddingmaterial
15.11
15.11.1
PD 6687-2 table 3
BS EN 1992-1-1 10.9.4.3(3)
BS EN 1992-1-1 10.9.5.2(2)
106
15.12
BS EN 1992-1-1 10.9.5.1(4)
BS EN 1992-1-1 10.9.5.2(1)
BS EN 1992-1-1 10.9.4.7(1)
BS EN 1992-1-1 10.9.5.2(3)
BS EN 1992-1-1 fig. 10.6
Bearings
Bearingsshallbedesignedanddetailedtoensurecorrectpositioningtaking intoaccounttheproductionandassemblingdeviations.
Thenominallength,a,ofasimplebearingasshowninFigure15.11maybecalculatedas:
++= Da22a a1 +a2 +a3 Da3
2
where a1 = netbearinglengthwithregardtobearingstressa1=FEd/(b1 fRd)butnotlessthan
minimumvaluesinTable15.4 FEd = designvalueofsupportreaction b1 = netbearingwidth(seebelow) fRd = designvalueofbearingstrength(seeSection15.11.1) a2 = distanceassumedineffectivebeyondouterendofsupportingmember,seeFigure
15.11andTable15.5 a3 = similardistanceforsupportedmember,seeFigure15.11andTable15.6 Da2 = allowancefordeviationsforthedistancebetweensupportingmembers,seeTable
15.7 Da3 = allowancefordeviationsforthelengthofsupportingmember = ln/2500 ln = lengthofmember
Theeffectivebearinglengtha1iscontrolledbyadistance,d,(seeFigure15.12)fromtheedgeoftherespectiveelements
where di = ci+Daiwithhorizontalloopsorotherwiseend-anchoredbars di = ci+Dai+riwithverticallybentbars
where ci = concretecover Dai = deviation ri = bendradius
Ifmeasuresaretakentoobtainauniformdistributionofthebearingpressure,e.g.withmortar,neopreneorsimilarpads,thedesignbearingwidthb1maybetakenastheactualwidthofthebearing.Otherwise,and intheabsenceofamoreaccurateanalysis,b1shouldnotbegreaterthanto600mm.
a) Elevation b) Plan
Da3a3
b1
a1
a1
a+ Da2a2+
Figure 15.11Example of bearing with definitions
107
Detailing–particularrequirements
Figure 15.12Example of
detailing of reinforcement
in support
di ci
ri
ri
> a1 + Da3
ci di> a1 + Da2
Table 15.4Minimum value of
a1 (mm)
Relative bearing stress, sEd / fcd ≤0.15 0.15 – 0.4 >0.4
Line supports (floors, roofs) 25 30 40
Ribbed floors and purlins 55 70 80
Concentrated supports (beams) 90 110 140
Table 15.5Distance a2 (mm) assumed ineffective from outer end of supporting member
Support material and type Relative bearing stress, sEd / fcd
≤0.15 0.15 – 0.4 >0.4
Steel line
concentrated
0
5
0
10
10
15
Reinforced concrete ≥ C30 line
concentrated
0
10
10
15
15
25
Plain concrete and reinforced concrete < C30 line
concentrated
10
15
15
25
25
35
Brickwork line
concentrated
10
20
15
25
a
a
KeyaConcretepadstoneshouldbeusedinthesecases
Table 15.6Distance a3 (mm) assumed ineffective beyond outer end of supported member
Detailing of reinforcement Support
Line Concentrated
Continuous bars over support (restrained or not) 0 0
Straight bars, horizontal, close to end of member 5 15,butnotlessthanendcover
Tendons or straight bars exposed at end of member
5 15
Vertical loop reinforcement 15 Endcover+innerradiusofbending
BS EN 1992-1-1fig.10.5
BS EN 1992-1-1table 10.2
BS EN 1992-1-1table 10.3
BS EN 1992-1-1table 10.4
108
BS EN 1992-1-1table 10.5
Table 15.7 Allowance Da2 for tolerances for the clear distance between the faces of the supports
Support material Da2
Steel or precast concrete 10≤l/1200≤30mm
Brickwork or cast in-situ concrete 15≤l/1200+5≤40mm
Notel=spanlength
109
Designfortheexecutionstages
16 Design for the execution stages
Forbridgesbuilt instages,accountoftheconstructionprocedureshouldbeconsideredatserviceabilityandultimatelimitstates.
Serviceabilitycriteriaforthecompletedstructureneednotbeappliedtointermediateexecutionstages,providedthatdurabilityandfinalappearanceofthecompletedstructurearenotaffected(e.g. deformations). Even for bridges or elements of bridges in which the limit-state ofdecompressionischeckedunderthequasi-permanentorfrequentcombinationofactionsonthe completed structure, tensile stresses less than 1.0 fctm(t) under the quasi-permanentcombinationofactionsduringexecutionarepermitted.Forbridgesorelementsofbridges inwhich the limit-state of cracking is checked under frequent combination on the completedstructure,thelimitstateofcrackingshouldbeverifiedunderthequasi-permanentcombinationofactionsduringexecution.
BS EN 1992-2113
BS EN 1992-2113.3.2
110
Design aids
Thefollowingtext,tablesandfigureshavebeenderivedfromEurocode2andareprovidedasanaidtodesignersintheUK.
Design for bending
Determinewhether■■ K ≤K’ornot(i.e.whetherunder-reinforcedornot). where K = MEd/(bd2fck)
where d= effectivedepth=h–cover–flink–f/2 b= widthofsection
ForrectangularsectionsK'maybedeterminedfromTable17.1or,forslabsonly,Table17.2maybeused.K'isdependentontheconcretestrengthandtheredistributionratioused.
Fornon-rectangularsectionx/dlimitsgiveninTable17.1maybeused.
If■■ K≤K',sectionisunder-reinforced.
Forrectangularsections:
As1=MEd/fydz
where As1 = areaoftensilereinforcement MEd= designmoment fyd = fyk/gS=500/1.15=434.8MPa z = d[0.5+0.5(1–3.53K/n)0.5]≤0.95d n = factordefiningeffectivestrength = 1.0–( fck–50)/200(seeTable6.1)
Forflangedbeamswherex<1.25hf,
As1= MEd/fydz x = depthtoneutralaxis hf = thicknessofflange For flanged beams where x ≥ 1.25hf, refer to How to design concrete structures using
Eurocode 2: Beams [25]
If■■ K>K',sectionisover-reinforced andrequirescompressionreinforcement.
As2=(MEd–M'Ed)/fsc(d–d2)
where As2 = compressionreinforcement M'Ed = K'bd2fck fsc = 700(xu–d2)/xu≤fyd
where d2 = effectivedepthtocompressionreinforcement xu = (d–l/z)d d = redistributionratio
Whenfyk=500MPa,fsc=fydunlessd2/xu≥0.379.
TotalareaoftensionsteelAs1=M'Ed /(fydz)+As2fsc/fyd
17
17.1
Section 4
111
Designaids
Table 17.1Limiting values of K' and xu/d
Percentage redistribution
d ( Redistribution ratio)
fck 50 55 60 70
n 1.000 0.975 0.950 0.900
l 0.800 0.788 0.775 0.750
ecu2 0.0035 0.0031 0.0029 0.0027
k1 or k3 0.44 0.54 0.54 0.54
k2 = k4 1.251 1.310 1.357 1.409
0 1.00 K' 0.167 0.132 0.123 0.110
xu /d 0.448 0.351 0.339 0.326
5 0.95 K' 0.155 0.119 0.111 0.099
xu /d 0.408 0.313 0.302 0.291
10 0.90 K' 0.142 0.107 0.099 0.088
xu/d 0.368 0.275 0.265 0.256
15 0.85 K' 0.129 0.093 0.087 0.077
xu /d 0.328 0.237 0.228 0.220
Table 17.2Limiting values of K' and xu/d for slabs
Percentage redistribution
d ( Redistribution ratio)
fck 50 55 60 70
n 1.000 0.975 0.950 0.900
l 0.800 0.788 0.775 0.750
ecu2 0.0035 0.0031 0.0029 0.0027
k1 or k3 0.4 0.4 0.4 0.4
k2 = k4 1.000 1.048 1.086 1.127
0 1.00 K' 0.207 0.193 0.181 0.163
xu /d 0.600 0.573 0.553 0.532
5 0.95 K' 0.194 0.181 0.170 0.152
xu /d 0.550 0.525 0.507 0.488
10 0.90 K' 0.181 0.169 0.158 0.141
xu/d 0.500 0.477 0.461 0.444
15 0.85 K' 0.167 0.155 0.145 0.130
xu /d 0.450 0.429 0.415 0.399
20 0.80 K' 0.152 0.141 0.132 0.118
xu /d 0.400 0.382 0.368 0.355
25 0.75 K' 0.136 0.126 0.118 0.105
xu /d 0.350 0.334 0.322 0.311
30 0.70 K' 0.120 0.111 0.103 0.092
xu /d 0.300 0.286 0.276 0.266
112
17.2
17.2.1
17.2.2
17.2.3
Design for beam shear
Requirement for shear reinforcement
IfvEd>vRd,cthenshearreinforcementisrequired
where vEd = VEd/bwd,forsectionswithoutshearreinforcement(i.e.slabs) vRd,c = shearresistancewithoutshearreinforcement,fromTable17.3
Table 17.3Shear resistance without shear reinforcement, vRd,c (MPa)
rl = Asl/bwd Effective depth d (mm)
≤ 200 225 250 275 300 350 400 450 500 600 750
0.25% 0.54 0.52 0.50 0.48 0.47 0.45 0.43 0.41 0.40 0.38 0.36
0.50% 0.59 0.57 0.56 0.55 0.54 0.52 0.51 0.49 0.48 0.47 0.45
0.75% 0.68 0.66 0.64 0.63 0.62 0.59 0.58 0.56 0.55 0.53 0.51
1.00% 0.75 0.72 0.71 0.69 0.68 0.65 0.64 0.62 0.61 0.59 0.57
1.25% 0.80 0.78 0.76 0.74 0.73 0.71 0.69 0.67 0.66 0.63 0.61
1.50% 0.85 0.83 0.81 0.79 0.78 0.75 0.73 0.71 0.70 0.67 0.65
1.75% 0.90 0.87 0.85 0.83 0.82 0.79 0.77 0.75 0.73 0.71 0.68
≥2.00% 0.94 0.91 0.89 0.87 0.85 0.82 0.80 0.78 0.77 0.74 0.71
Notes1 TablederivedfromBSEN1992-1-1andUKNationalAnnex.
2 Tablecreatedforfck=30MPaassumingverticallinks.
3 Forrl≥0.4%and fck = 25MPa,applyfactorof0.94 fck = 40MPa,applyfactorof1.10 fck ≥ 50MPa,applyfactorof1.19
fck = 35MPa,applyfactorof1.05 fck = 45MPa,applyfactorof1.14
Section capacity check
IfvEd,z>vRd,maxthensectionsizeisinadequate
where vEd,z = VEd/bwz=VEd/bw0.9d,forsectionswithshearreinforcement vRd,max = capacityofconcretestrutsexpressedasastressintheverticalplane = VRd,max/bwz = VRd,max/bw0.9d
vRd,maxcanbedeterminedfromTable17.4,initiallycheckingatcoty=2.5.Shoulditberequired,agreaterresistancemaybeassumedbyusingalargerstrutangle,y.
Shear reinforcement design
Asw/s≥vEd,zbw/fywdcoty
where Asw = areaofshearreinforcement(verticallinksassumed) s = spacingofshearreinforcement vEd,z = VEd/bwz,asbefore bw = breadthoftheweb fywd = fywk/gS=designyieldstrengthofshearreinforcement
Alternatively,Asw/spermetrewidthofbwmaybedeterminedfromFigure17.1a)or17.1b)asindicatedbythebluearrowsinFigure17.1a).Thesefiguresmayalsobeusedtoestimatethevalueofcoty.
Section 7.3.2
Section 7.3.3
Section 7.2
113
Designaids
Beamsaresubjecttoaminimumshearlinkprovision.Assumingverticallinks,Asw,min/sbw≥0.08fck
0.5/fyk(seeTable17.5).
Table 17.4Capacity of concrete struts expressed as a stress, vRd,max, where z = 0.9d
fck vRd,max (MPa) v
cot y 2.50 2.14 1.73 1.43 1.19 1.00
y 21.8º 25º 30º 35º 40º 45º
25 3.10 3.45 3.90 4.23 4.43 4.50 0.540
30 3.64 4.04 4.57 4.96 5.20 5.28 0.528
35 4.15 4.61 5.21 5.66 5.93 6.02 0.516
40 4.63 5.15 5.82 6.31 6.62 6.72 0.504
45 5.09 5.65 6.39 6.93 7.27 7.38 0.492
≥50 5.52 6.13 6.93 7.52 7.88 8.00 0.480
Notes1 TablederivedfromBSEN1992-1-1andUKNationalAnnexassumingverticallinks,i.e.cota=0
2 v=0.6[1–(fck/250)]
3 vRd,max=vfcd(coty+cota)/(1+cot2y)
Table 17.5Values of Asw,min/sbw × 103 for beams for vertical links and fyk = 500 MPa
Concrete class C20/25 C25/30 C30/37 C35/45 C40/50 C45/55 ≥C50/60
Asw,min /sbwx103 0.72 0.80 0.88 0.95 1.01 1.07 1.13
4.0
3.0
2.0
5.0
6.0
7.0
8.0
0 2 4 6 8 10 12 14
C35/45
C40/50
C45/55
0.0
1.0
2.14 1.73 1.43
1.19
1.00
SeeFig.17.1b)
Asw/srequired per metre width of bw
fywk= 500 MPa
vRd,maxforcoty=2.5
v Ed,z
(M
Pa)
C30/37
C20/25
C25/30
≥C50/60
Figure 17.1a)Diagram to determine Asw/s required (for beams with high shear stress)
Section 15.2.6
114
C20/25C25/30C30/37
C30/37
C35/45C40/50C45/55C50/60
4.0
3.0
2.0
1.0
0.00 1 2 3 4
fywk = 500 MPa
Asw,min/sforbeams
RangeofvRd,cforranged=200mm,r=2.0%tod=750mm,r=0.5%
C25/30
Asw/srequired per metre width of bw
v Ed,z
(M
Pa)
C20/25
Figure 17.1b)Diagram to determine Asw/s required (for slabs and beams with low shear stress)
Design for punching shear
Determine if punching shear reinforcement is required, initially at u1, then if necessary atsubsequentperimeters,ui.IfvEd>vRd,cthenpunchingshearreinforcementisrequired
where vEd = bVEd/uid
where b = factordealingwitheccentricity(seeSection8.2) VEd = designvalueofappliedshearforce ui = lengthoftheperimeterunderconsideration(seeSections8.3,8.7and15.4.3) d = meaneffectivedepth vRd,c = shearresistancewithoutshearreinforcement(seeTable17.3)
Forverticalshearreinforcement
(Asw/sr)=u1(vEd–0.75vRd,c)/(1.5fywd,ef)
where Asw = areaofshearreinforcementinoneperimeteraroundthecolumn. ForAsw,minseeSection15.4.3 sr = radialspacingofperimetersofshearreinforcement u1 = basiccontrolperimeter(seeFigures8.3and8.4) fywd,ef = effectivedesignstrengthofreinforcement=(250+0.25d)≤fywd.ForClass500
shearreinforcementseeTable17.6
Table 17.6Values of fywd, ef for Class 500 reinforcement
d 150 200 250 300 350 400 450
fywd,ef 287.5 300 312.5 325 337.5 350 362.5
17.3
Section 8.21
Section 8.5
Section 15.4.3
115
Designaids
17.4
17.4.1
17.4.2
Design for axial load and bending
General
Incolumns,designmomentsMEdanddesignappliedaxialforceNEdshouldbederivedfromanalysis,considerationofimperfectionsand,wherenecessary,2ndordereffects(seeSection5.6).
Design by calculation
Assumingtwolayersofreinforcement,As1andAs2,thetotalareaofsteelrequiredinacolumn,As,maybecalculatedasshownbelow.
Foraxialload■■
AsN/2 = (NEd–accnfckbdc/gC)/(ssc–sst)
where AsN= totalareaofreinforcementrequiredtoresistaxialloadusingthismethod. AsN= As1+As2andAs1=As2
where As1(As2) = areaofreinforcementinlayer1(layer2)(seeFigure6.3) NEd= designvalueofaxialforce acc = 0.85 n = 1for≤C50/60(seeTable6.1whenfck>50) b = breadthofsection dc = effectivedepthofconcreteincompression=lx≤h
where l = 0.8for≤C50/60(seeTable6.1whenfck>50) x = depthtoneutralaxis h = heightofsection gC = 1.5 ssc,(sst)= stressincompression(andtension)reinforcement
Formoment■■
AsM=
MEd–accnfckbdc(h/2–dc/2)/gC
2 (h/2–d2)(ssc+sst)
where AsM = totalareaofreinforcementrequiredtoresistmomentusingthismethod AsM = As1+As2andAs1=As2
Solution:iterate■■ xsuchthatAsN=AsM.
Section 5.6
Section 6.2.2
116
17.4.3 Column charts
AlternativelyAsmaybeestimatedfromcolumncharts.
Figures17.2a)toe)givenon-dimensionaldesignchartsforsymmetricallyreinforcedrectangularcolumnswherereinforcementisassumedtobeconcentratedinthecorners.
Inthesecharts:acc = 0.85fck ≤ 50MPa
Simplifiedstressblockassumed.
As = totalareaofreinforcementrequired = (As fyk/bh fck)bh fck/fykwhere (As fyk/bh fck) is derived from the appropriate design chart interpolating as necessary
betweenchartsforthevalueofd2/hforthesection.
Wherereinforcementisnotconcentratedinthecorners,aconservativeapproachistocalculateaneffectivevalueofd2asillustratedinFigures17a)toe).d2=effectivedepthtosteelinlayer2.
Figures17.3a)toe)givenon-dimensionaldesignchartsforcircularcolumns.
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.0
1.3
1.2
1.1
1.0
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
00 0.05 0.10 0.15 0.20 0.25 0.30 0.35 0.40 0.45
0
0.10.2
0.3
0.40.5
0.60.7
0.8
0.91.0
Af
bhf
syk
c k
/
K r = 0.2
Figure 15.5(a)Rectangular columns / = 0.05d h2
h/2
h
d 2
Centroid of bars inhalf section
Ratio d2/h = 0.05
N/ Ed
/bhf
ck
MEd/bh2fck
Figure 17.2a)Rectangular columns (fck ≤ 50 MPa, fyk = 500 MPa) d2/h = 0.05
117
Designaids
h/2
h
d 2
Centroid of bars inhalf section
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.3
1.2
1.1
1.0
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
00 0.05 0.10 0.15 0.20 0.25 0.30 0.35 0.40 0.45
K r =1
K r = 0.2
0
0.10.2
0.3
0.40.5
0.6
0.7
0.80.9
1.0
Figure 15.5(b)Rectangular columns / = 0.10d h2
Af
bhf
syk
/ck
Ratio d2/h = 0.10
NEd
/bhf
ck
MEd/bh2fck
Figure 17.2b)Rectangular columns (fck ≤ 50 MPa, fyk = 500 MPa) d2/h = 0.10
h/2
h
d 2
Centroid of bars inhalf section
0.3
0.4
0.5
0.6
0.7
0.8
0.9
0
0.10.2
0.30.4
0.5
0.7
0.9
1.0
1.3
1.2
1.1
1.0
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
00 0.05 0.10 0.15 0.20 0.25 0.30 0.35 0.40
Af
bhf
syk
c k
/
K r =1
K r = 0.2
Figure 15.5(c)Rectangular columns / = 0.15d h2
0.6
0.8
Ratio d2/h = 0.15
MEd/bh2fck
N/ Ed
/bhf
ck
Figure 17.2c)Rectangular columns (fck ≤ 50 MPa, fyk = 500 MPa) d2/h = 0.15
118
h/2
h
d 2
Centroid of bars inhalf section
0 0.05 0.10 0.15 0.20 0.25 0.30 0.350
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.0
1.2
1.1
1.3
0.3
0.4
0.5
0.6
0.7
0.8
0.9
Af
bhf
syk
c k
/
Ratio d2/h = 0.20
Figure 15.4(d)Rectangular columns / = 0.20d h2
K r = 1
K r = 0.2
00.1
0.2
0.3
0.4
0.5
0.60.7
0.8
0.9
1.0
N/ Ed
/bhf
ck
MEd/bh2fck
Figure 17.2d)Rectangular columns (fck ≤ 50 MPa, fyk = 500 MPa) d2/h = 0.20
Af
bhf
syk
c k
/
Figure 15.5(e)Rectangular columns / = 0.25d h2
K r = 0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.3
1.2
1.1
1.0
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
00 0.05 0.10 0.15 0.20 0.25 0.30
1.00.9
0. 80.7
0.60.5
0.40.3
0.20.1
0
K r = 1
h/2
h
d 2
Centroid of bars inhalf section
N/ Ed
/bhf
ck
MEd/bh2fck
Ratio d2/h = 0.25
Figure 17.2e)Rectangular columns (fck ≤ 50 MPa, fyk = 500 MPa) d2/h = 0.25
119
Designaids
Kr =1
0.9
0.8
0.7
0.6
0.5
0.4
0.31.0
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
0
0.2
1.2
1.1
1.0
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
00 0.01 0.02 0.03 0.04 0.05 0.06 0.07
0.9
dh
File Concise EurocodeCircular Columns 0.6v1 10.11.08
As fyk/h2fck Ratio d/h = 0.6
NEd
/h2
f ck
MEd / h3fck
Figure 17.3a)Rectangular columns (fck ≤ 50 MPa, fyk = 500 MPa) d2/h = 0.6
1.2
1.1
1.0
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
00 0.02 0.04 0.06 0.08 0.10 0.12
0.2
0.3
0.4
0.5
0.6
0.7
0.8
1.0
0.9
0.8
0.7
0.6
0.5
0.4
0
0.10.2
0.3
File Concise Eurocode
d h
Ratio d/h = 0.7
NEd
/h2
f ck
MEd / h3fck
Kr =1
As fyk/h2fck
Figure 17.3b)Rectangular columns (fck ≤ 50 MPa, fyk = 500 MPa) d2/h = 0.7
120
d h
1.2
1.1
1.0
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
00 0.02 0.04 0.06 0.08 0.10 0.12 0.14 0.16 0.18 0.20
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.0
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
0
Ratio d/h = 0.8As fyk/h2fck
Kr =1
NEd
/h2
f ck
MEd / h3fck
Figure 17.3c)Rectangular columns (fck ≤ 50 MPa, fyk = 500 MPa) d2/h = 0.8
d h
0.2
0.31.0
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0
0.4
0.5
0.6
0.7
0.8
0.9
0 0.05 0.10 0.15 0.20 0.25
1.2
1.1
1.0
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
0
0.1
File Concise EurocodeCircular Columns 0.85
Ratio d/h = 0.85
Kr =1
As fyk/h2fck
NEd
/h2
f ck
MEd / h3fck
Figure 17.3d)Rectangular columns (fck ≤ 50 MPa, fyk = 500 MPa) d2/h = 0.85
121
Designaids
d h
0.05 0.10 0.15 0.20 0.25 0.30
0.7
0.2
0.3
0.4
0.5
0.6
0.8
0.9
1.0
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
0
1.2
1.1
1.0
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
00
File Concise EurocodeCircular Columns 0.9v1 10.11.08
Ratio d/h = 0.9
Kr =1
As fyk/h2fck
NEd
/h2
f ck
MEd / h3fck
Figure 17.3e)Rectangular columns (fck ≤ 50 MPa, fyk = 500 MPa) d2/h = 0.9
122
18 References
1 BRITISHSTANDARDSINSTITUTION.BSEN1992-1-1,Eurocode2–Design of concrete structures Part1-1: General rules and rules for buildings. BSI,2004,incorporatingcorrigendumdated12-11-2007.1a NationalAnnextoEurocode2–Part1-1.BSI,2005.
2 BRITISHSTANDARDSINSTITUTION.BSEN1992-2,Eurocode2–Design of concrete structures Part2: Concrete bridges – Design and detailing rules. BSI,2005,incorporatingcorrigendumdated12-11-2007.2a NationalAnnextoEurocode2–Part2.BSI,2007.
3 BRITISHSTANDARDSINSTITUTION.PD6687-2Recommendations for the design of structures to BS EN 1992-2: 2005.BSI,2008.
4 WOOD,RH.Thereinforcementofslabsinaccordancewithapre-determinedfieldofmoments. Concrete, 1968,No.2,pp.69–76.
5 DENTON,SR&BURGOYNE,CJ.Theassessmentofreinforcedconcreteslabs. The Structural Engineer,7thMay1996,Vol.74,No.9,pp.147–152.
6 BRITISHSTANDARDSINSTITUTION.PD6687Background paper to the UK National Annexes BS EN 1992-1.BSI,2006.
7 BRITISHSTANDARDSINSTITUTION.BSEN1990,Eurocode:Basis of structural design. BSI,2002,incorporatingamendmentNo.1.7a NationalAnnextoEurocode.BSI,2004,incorporatingamendmentNo.1.
8 BRITISHSTANDARDSINSTITUTION.BS8500-1:Concrete –Complementary British Standard to BS EN 206-1 – Part 1: Method of specifying and guidance to the specifier. BSI,2006.
9 BRITISHSTANDARDSINSTITUTION.BSEN1991,Eurocode1:Actions on structures (10parts).BSI,2002–2006.9a NationalAnnexestoEurocode1.BSI,2005 –2009andinpreparation.
10 BRITISHSTANDARDSINSTITUTION.ENV13670-1:2008:Execution of concrete structures: Common.BSI,2000.
11 BRITISHSTANDARDSINSTITUTION.BSEN13670.Execution of concrete structures.BSI,due2009.
12 BRITISHSTANDARDSINSTITUTION.BSEN1997,Eurocode7:Geotechnical design – Part 1. General rules.BSI,2004.12a NationalAnnextoEurocode7–Part1.BSI,2007.
13 BRITISHSTANDARDSINSTITUTION.PD6694-1Recommendations for the design of structures subject to traffic loading to BS EN 1997-1:2004.BSI,due2009.
14 BRITISHSTANDARDSINSTITUTION.BSEN206-1.Concrete – Part 1: Specification, performance, production and conformity. BSI,2000.
15 BRITISHSTANDARDSINSTITUTION.BSEN197-1Cement – Composition, specifications and conformity criteria for common cements.BSI,2000.
16 BRITISHSTANDARDSINSTITUTION.BS4449:Steel for the reinforcement of concrete – Weldable reinforcing steel – Bar, coil and decoiled product – Specification. BSI,2005.
17 BRITISHSTANDARDSINSTITUTION.BSEN10080:Steel for the reinforcement of concrete – Weldable reinforcing steel – General. BSI,2005.
18 BRITISHSTANDARDSINSTITUTION.BS5896.High tensile steel wire and strand for the prestressing of concrete. BSI,1980,incorporatingamendmentNo.1.
19 BUILDINGRESEARCHESTABLISHMENT.Concrete in aggressive ground. BRESpecialDigest1.BRE,2005.
123
References
20 HENDY,CR&SMITH,DA.Designers guide to EN 1992–2. ThomasTelford,2007.
21 ENV1992-1-1:Eurocode2:Design of concrete structures - Part 1-1: General rules and rules for buildings.BSI,1992(supersededbyreference1).
22 INTERNATIONALSTANDARDSORGANISATION,ISO/FDIS.17660-2:Welding – Welding of reinforcing steel – Part 2: Non load-bearing welded joints.ISO,2005.
23 BRITISHSTANDARDSINSTITUTION.BSEN1536:Execution of special geotechncial work – Bored piles.BSI,2000.
24 BRITISHSTANDARDSINSTITUTION.BS5400:Steel, concrete and composite bridges – Part 4: Code of Practice for design of concrete bridges.BSI,1990.
25 BROOKER,Oetal.How to design concrete structures using Eurocode 2. TheConcreteCentre,2006.
3
Guide to presentation
Grey shaded text, tables and figures
Modified Eurocode 2 text and additional text, derived formulae, tables and illustrations not from Eurocode 2
Yellow shaded text, tables and figures
Additional text from PD 6687[6] or PD 6687-2[3]
BS EN 1992-1-1 6.4.4
Relevant code and clauses or figure numbers
BS EN 1992-1-1 NA From the relevant UK National Annex
BS EN 1992-1-1 6.4.4 & NA From both Eurocode 2-1-1 and UK National Annex
Section 5.2 Relevant parts of this publication
1.0 Nationally Determined Parameter. UK values have been used throughout
4
Concise Eurocode 2 for Bridges
This publication summarises the material that will be commonly used in the design of reinforced and prestressed concrete bridges using Eurocode 2.
With extensive clause referencing, readers are guided through Eurocode 2, other relevant European standards and non-contradictory complementary information. The publication, which includes design aids, aims to help designers with the transition to design using Eurocodes.
Concise Eurocode 2 for Bridges is part of a range of resources available from the cement and concrete industry to assist engineers with the design of a variety of concrete bridges. For more information visit www.concretecentre.com
Owen Brooker is senior structural engineer for The Concrete Centre. He is author of several publications, including the well received series How to design concrete structures using Eurocode 2. He regularly lectures and provides training to structural engineers, particularly on the application of Eurocode 2.
Paul Jackson is a technical director of Gifford, which he joined from BCA in 1988. He has worked on bridge design, assessment, construction, strengthening and research. He has contributed extensively to codes of practice and is currently a member of the BSI committee for bridges and convenor of its working group for concrete bridges. He served on the project team for EN 1992-2.
Stephen Salim is a senior engineer with Gifford. He has worked on bridge assessment, feasibility studies, design, construction supervision and research. He was also involved in the calibration work of BS EN 1992-2; some of the proposals arising from this work were adopted in the UK National Annex.
CCIP-038Published 2009ISBN 978-1-904818-82-3Price Group P© MPA – The Concrete Centre
Riverside House, 4 Meadows Business Park,Station Approach, Blackwater, Camberley, Surrey, GU17 9ABTel: +44 (0)1276 606800 Fax: +44 (0)1276 606801www.concretecentre.com