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Symposium in honour of Gianpietro Del Piero Sperlonga September 30th and October 1st 2011. The static theorem of limit analysis for masonry panels M. Lucchesi , M. ilhav N. Zani Š ý,

Sperlonga 2011

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Page 1: Sperlonga 2011

Symposium in honour of Gianpietro Del Piero

Sperlonga

September 30th and October 1st 2011.

The static theorem of limit analysis for masonrypanels

M. Lucchesi , M. ilhav N. ZaniŠ ý,

Page 2: Sperlonga 2011

2

Constitutive equations

In order to characterize a masonry-like material we assume

that the stress must be negative semidefinite and that the

strain is the sum of two parts: the former depends linearly

on the stress, the letter is orthogonal to the stress and

positive semidefinite,

X − Sym

I I Iœ / 0

I0 − Sym

X Iœ Ò Ó‚ /

I X0 † œ !

where I ? ? ?( ) œ Ðf f Ñ"

#T

is the infinitesimal strain and is symmetric and positive‚

definite, i.e.,

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E E E E" # # "† Ò Ó œ † Ò Óß‚ ‚

E E E E !† Ò Ó ! − ß Á‚ for each Sym

Proposition

For each Sym there exists a unique tripletI −

Ð ß ß ÑX I I/ 0 that satisfies the constitutive equation.

Moreover, a masonry-like material is hyperelastic.

We write

AÐ Ñ œ Ð Ñ †I X I I"#

for the stored energy.

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Notations

H reference configuration of the body

` œ ß œ gH W f W f such that

u? ! displacement field, such that lWœ

= À Äf ‘$ surface traction

body force, À ÄH ‘$

X À ÄH Sym stress tensor

D

Sb

s

Ω

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Limit analysis

The limit analysis deals with a family of loads that_ -Ð Ñ

depend linearly on a scalar parameter ,- ‘−

_ - - -Ð Ñ œ Ð ß Ñ œ Ð ß Ñ, = , , = =- -! " ! "

, =! !, permanent part of the load

variable part of the load, =" "ß

loading multiplier-

, ,! " and are supposed to be square integrable functions on

H, and are supposed to be square integrable functions= =! "

on .f

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Let

Z œ Ö − [ Ð ß Ñ À œ ×@ @ !"ß# $H ‘ W a.e. on

be the Sobolev space of all valued maps such that and‘$ @

the distributional derivative of are square integrablef@ @

on .H

For each we define the Ð ß Ñ − ‚ Z- ‘@ potential energy

of the body

MÐ ß Ñ œ AÐ Ð Ñ.Z † .Z † .E- @ I @ @ , @ =( ( (H H f

- -

where

(H

AÐ Ð Ñ.ZI @

is the strain energy and

Ð Ñß œ † .Z † .E_ - @ @ , @ =( (H f

- -

is the work of the loads.

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Moreover, we define the infimum energy

M Ð Ñ œ ÖMÐ ß Ñ À − Z ×Þ! - -inf @ @

Proposition

(i) The functional is ,M À Ä Ö _×! ‘ ‘ concave

M Ð+ Ð" +Ñ Ñ   +M Ð Ñ Ð" +ÑM Ð Ñ! ! !- . - .

for every , and .- . ‘− + − Ò!ß "Ó

Therefore, the set

A - ‘ -À œ Ö − À M Ð Ñ _×!

is an interval.

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(ii) The functional is ,M! upper semicontinuous

M Ð Ñ   M Ð Ñ! ! 55Ä_

- -lim sup

for every and every sequence .- ‘ - -− Ä5

We interpret the elements of as loading multipliers forA

which the loads are , i.e. the body does not_ -Ð Ñ safe

collapse.

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Each finite endpoint of the interval is called a- A-

collapse multiplier with the interpretation that for - -œ -

or at least for arbitrarily close to outside the body- - A-

collapses.

We say that a stress field is ifX admissible

X − P Ð ß Ñ# H Sym

and that ifX , =equilibrates the loads _ -Ð Ñ œ Ð ß Ñ- -

( ( (H H f

X I @ @ , @ =† Ð Ñ.Z œ † .Z † .E- -

for every .@ − Z

We say that the loads are if there exists a_ -Ð Ñ compatible

stress field that is admissible and equilibrates X _ -Ð ÑÞ

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Proposition (Static theorem of the limit analysis)

The loads are compatible if and only if_ -Ð Ñ

M Ð Ñ _! - .

That is the loads are safe (i.e. ) if and only if_ - - AÐ Ñ −

there exist a stress field whichX

(i) is square integrable,

(ii) takes its values in Sym ,

(iii) equilibrates the loads ._ -Ð Ñ

Page 11: Sperlonga 2011

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Rectangular panels

In the study of the static of masonry panels we verify that

the problem of finding negative semidefinite stress fields

that equilibrate the loads is considerably simplified if

instead of stress fields represented by square integrable

functions we allow the presence of curves of concentrated

stress.

xy

op

h

λq

γΩ

Ω

λ

λ

λ

+

γλ

b

Page 12: Sperlonga 2011

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Example

In the following example, firstly, we will obtain a stress

field which is a measure, whose divergence is a measure,

that equilibrate the loads in a weak sense. Then we will see

a procedure that, starting from this singular stress field,

allow us to determine a stress field which is admissible and

equilibrates the loads in the classical sense.

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x

y

O

γ

λ

λ

p

H ‘œ Ð!ß ,Ñ ‚ Ð!ß 2Ñ § ß#

W œ Ð!ßFÑ ‚ Ö2×ß

f H Wœ ` Ï ß

, !- œ ß

= <43

!

-Ð Ñ œ: Ð!ß ,Ñ ‚ Ö!×

ß Ö!× ‚ Ð!ß 2Ñ

ÚÛÜ

, on on elsewhere

-

where and .: !ß ! œ ÐBß CÑ- <

Page 14: Sperlonga 2011

14

x

y

O

γ

λ

λ

p

Ωλ+

Ωλ−

a

The singularity curve can be obtained by imposing the#-

equilibrium of the shaded rectangular region with the

respect to the rotation about its left lower corner. We

obtain

#- œ ÖÐBß CÑ − À C œ B×:

H-

Ê

Page 15: Sperlonga 2011

15

which divides into the two regions ,H H„-

H H-+

- œ ÖÐBß CÑ − À C B×:Ê ,

H H-

- œ ÖÐBß CÑ − À C B×Þ:Ê

The singularity curve has to be wholly contained into#-

the region and this impliesH

! - --

with

--

#

#œ Þ

:,

2

Page 16: Sperlonga 2011

16

For the regular part of the stress field (defined outsideX<-

#-) we take

X <4 4 <

3 3 <<

--

-Ð Ñ œ : Œ −

Œ − Þœ if

if H

- H+

The stress field defined on can be obtained by imposing#-

the equilibrium of the shaded rectangular region with the

respect to the translation. We obtain

X << <

<=-Ð Ñ œ : Þ

ŒÈ k k-

We note that is the unit tangent vector to .<

<k k #-

Page 17: Sperlonga 2011

17

The stress field

T- - -œ X X< =

has to be interpreted as a . That is,tensor valued measure

a function defined on the system of all Borel subsets of H

which takes its values in Sym and is countably additive,

T T- -Œ !3œ"

_

3 33œ"

_

E œ ÐE Ñ

for each sequence of pairwise disjoint (borelian) sets.

T- is the sum of an absolutely continuous part (with

respect to the area measure) with density and aX<-

singular, part concentrated on , with density . Both#- -X=

the densities and are regular functions.X X< =- -

Page 18: Sperlonga 2011

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We can prove that the stress measure weaklyT-

equilibrates the loads , that isÐ ß Ñ, =- -

( ( (H H f

I @ @ , @ =Ð Ñ. œ † .Z † .EßT - -

for any .@ − Z

Page 19: Sperlonga 2011

19

Integration of measures

By the static theorem of limit analysis, in order to assert

that the loads are we need an equilibrated_ -Ð Ñ compatible

stress field that is a square integrable function and then

equilibrated stress measures are not enough.

Now we describe a procedure that in certain cases allows

us to use the stress measure to determine a squareT-

integrable stress field . Crucial to this procedure is theX -

fact that both the loads and the admissibleÐ ß , Ñ=- -

equilibrating stress measure depend on a parameter .T- -

Page 20: Sperlonga 2011

20

x

y

o

μ

γμγμ+ε

γμ−ε

p

The idea is to take the average of the stress measure over

any set , where is sufficiently small.Ð ß Ñ !. % . % %

Averaging gives the measure

T Tœ . Þ"

#%( . %

. %

- -

Page 21: Sperlonga 2011

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It may happen that this measure, in contrast to , isT.

absolutely continuous with respect to the area measure with

a square integrable density.

For the previous example we obtain the following result.

If , then the loads are compatible. In fact! Ð Ñ- - _ .-

if then the measureÐ ß Ñ § Ð!ß Ñ. % . % --

T Tœ ."

#%( . %

. %

- -

is absolutely continuous with respect to the area

(Lebesgue) measure with density .X

X is a bounded admissible stress field on thatH

equilibrates the loads . We have_ .Ð Ñ

X X Xœ Þ< =

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22

The densities and can be explicitly calculated. InX X< =

fact, we have

X < X <<

<Ð Ñ œ Ð Ñ. œ

"

#%( . %

. %

- -

ÚÛÜ

: Œ − ÏE

Œ − ÏE

Ð# Œ Œ Ñ − E

4 4 <

3 3 <

3 3 4 4 <

if if if

H

. H

"

+-

-

% !Ñ Ð Ð Ñ Ð Ñ" < <

where

E œ ÖÐBß CÑ − À :B ÎC ×H . % . %# #

is the shaded area in the figure, and

!Ð Ñ œ Ð: B ÎC Ð"

#< # % % . % Ñ Ñß#

" . %Ð Ñ œ :Ð : B ÎC ÑÞ< # % %

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Moreover,

X <=

# #

Ð Ñ œ : B

!

ÚÛÜ %C

Œ − E%

< < <if

otherwise

It is easily to verify that the stress field

X X Xœ < =

is admissible, i.e. a square integrable function whichX

takes its values in Sym , and that it equilibrates the loads

_ .Ð Ñ,

X8 = X !œ œ. on , div in .f H

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Panels with opening

p

h1

h2

b2 b1 b2q

x

y

o

Ω 1

Ω 3

γ2

γ3

a

c

F1

e

d

A

B

C

Page 25: Sperlonga 2011

25

a

c

e

b2 b2b1

h1

h2

p

qc

b2

h1

h2

b1 b2

e

A

B

C

Page 26: Sperlonga 2011

26

a

pq

b1

h1

b2

h2

b2

c

a

b2

h2

h1

b1b2

Ι

A

B

C

Page 27: Sperlonga 2011

27

Panel under gravity

b

x

y

O

γ

λ

The panel is subjected to a side loads and its own gravity

= <3

!-Ð Ñ œ

!× ‚ Ð!ßLÑ on ,elsewhere.œ ˜-

Page 28: Sperlonga 2011

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The singularity curve is

# H -- œ ÐBß CÑ − À C œ -,B Î - œ "Î# $Î'Þš › È# ,

and

--#œ -,F ÎLÞ

X <4 4

3 3 3 4 4 4<

# #

-

-

-Ð Ñ œ

,C Œ ß

Œ ,B Œ ß, B

ÚÛÜ

in

in

H

- H-

with 3 4 3 4 4 3 œ Œ Œ Þ

Page 29: Sperlonga 2011

29

X > >=- - - -œ Œ ß5

with

5-Ð Ñ œ ,B B %C$

'<

È È # #

and

> <-Ð Ñ œÐBß #CÑ

B %CÈ # #

the unit tangent vector to .#-

Page 30: Sperlonga 2011

30

By integration we obtain

X <4 4

3 3 3 4 4 4W <

Ð Ñ œ ,C Œ ÏE ß

Œ ,B , B Î Œ ÏEßÐ Ñ Eß

ÚÛÜ

in in in

H

. - H

# #

-

-

where

E œ Ö œ ÐBß CÑ À ,-B ÎC − Ð ß Ñ×< # . & . &

and

W < 3 3Ð Ñ œ Ð# Ñ Ð Ñ Œ , B "

"#C #& . %" #

# %

#š’ “

’ “ ,BÐ Ñ , B

$C

# $

. & 3 4

’Š ‹ “ ›È$ & CÐ Ñ

# ' ,-B 68 , B ,CÐ Ñ Œ Þ

. &. %

## # 4 4

Page 31: Sperlonga 2011

31

References

[1] G. Del Piero Limit analysis and no-tension materials Int. J. Plasticity , 259-271 (1998)14[2] M. Lucchesi, N. Zani Some explicit solutions to equilibrium problem for masonry-like bodies Struc. Eng. Mech. , 295-316, (2003)16[3] M. Lucchesi, M. Silhavy, N. Zani A new class of equilibrated stress fields for no-tension bodies J. Mech. Mat. Struct. , 503-539, (2006)1[4] M. Lucchesi, M. Silhavy, N. Zani Integration of measures and admissible stress fields for masonry bodies J. Mech. Mat. Struct. , 675-696, (2008)3[5] M. Lucchesi, C. Padovani, M. Silhavy An energetic view of limit analysis for normal bodies Quart. Appl. Math , 713-746 (2010)68[6] M. Lucchesi, M. Silhavy, N. Zani Integration of parametric measures and the statics of masonry panels Ann. Solid Struct Mech. , 33-44, (2011)2