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Ran FENG1 and Ben YOUNG2
1 School of Civil Engineering, Hefei University of Technology, P.R. China
2 Department of Civil Engineering, The University of Hong Kong, Hong Kong
Stress Concentration Factors of Cold-Formed
Stainless Steel Tubular X-Joints
Stainless Steel In Structures: Fourth International Experts Seminar
6th-7th December 2012, Ascot, UK
Outline
Introduction
Hot Spot Stress Method
Experimental Investigation
Finite Element Analysis
Design Guidelines
Conclusions
Outline
Introduction
Hot Spot Stress Method
Experimental Investigation
Finite Element Analysis
Design Guidelines
Conclusions
Introduction
Weld
Brace
Chord
Geometric stress distribution in an
axially loaded CHS tubular X-joint
Nominal stress in brace
Peak stress in brace
Peak stress in chord
t0d 0
t1d 1
Stress Concentration
Outline
Introduction
Hot Spot Stress Method
Experimental Investigation
Finite Element Analysis
Design Guidelines
Conclusions
Hot Spot Stress Method
SCF FEA
Test
Weld
Brace
Chord
Geometric stress distribution in an
axially loaded CHS tubular X-joint
Nominal stress in brace
Peak stress in brace
Peak stress in chord
t0d 0
t1d 1
HSS
Hot Spot Location
t0
h0
b0
h1
b1
t1
Brace
Chord
45¡ã
A
BCD
EFH
I
G
Extrapolation Method SNCF
Distance from Weld Toe
Weld Toe
but ¡ Ý 4mm0.4t
Linear
Extrapolation
0.6t
SNCF Linear
Quadratic Extrapolation
1.0t
Measuring points
SNCF Quadratic
Outline
Introduction
Hot Spot Stress Method
Experimental Investigation
Finite Element Analysis
Design Guidelines
Conclusions
Test Specimens
/2/2
Welds
Seam weld
Welds
Brace
Brace
Chord
L 0
L 1
h1
w
w
h1
h1
t 1 b1
h0
r1
Seam weld
Weld
Brace
Brace
Chord
wt 0
b0 h0
b1
w
r0
Test Specimens
w
Specimen
Chord Brace Weld
(mm) (mm) (mm)
h0 b0 t0 r0 L0 h1 b1 t1 r1 L1 w β
XD-C140×3-B40×2 140.2 80.2 3.33 6.5 737 39.9 40.3 1.96 2.0 99 6.6 –– 0.50
XD-C140×3-B140×3 140.0 80.1 3.09 6.5 851 140.1 80.1 3.10 6.5 346 6.6 8.5 1.00
XH-C150×6-B150×6 150.3 150.5 5.75 6.0 902 150.3 150.3 5.84 6.0 368 9.2 15.5 1.00
XH-C110×4-B150×6 110.3 196.3 3.98 8.5 698 150.3 150.4 5.82 6.0 365 9.6 –– 0.77
XN-C40×4-B40×2 40.1 40.0 3.79 4.0 240 40.2 40.1 1.97 2.0 98 6.5 11.9 1.00
HSSN Measurement
Stress Concentration Measurement
Location of Strain Gauges h1
b0 b1
t 0
h0
b0
Brace
Chord
: Single element strain gauge for nominal strain at mid-length of brace member
: Strip strain gauges for hot spot strain (HSSN) at chord member
: Strip strain gauges for hot spot strain (HSSN) at brace member
28
28
2
8
Weld Toe Weld Toe
Brace
Chord
28
Test Rig and Procedure
Determination of SCF
nSNCF /
SNCFSCF2
//
1
1
HSSN perpendicular to weld toe
Nominal strain
Strain component parallel to weld toe
Determination of SCF
Hot spot
location
Axial compression force (kN)
Average
S/N
ratio
19.9 40.1 59.8 80.3 99.5
ξ┴ ξ// S/N ξ┴ ξ// S/N ξ┴ ξ// S/N ξ┴ ξ// S/N ξ┴ ξ// S/N
A -40.2 26.6 0.88 -121.6 53.4 0.95 -204.0 80.4 0.97 -295.6 113.6 0.97 -388.6 148.4 0.97 0.948
B 20.1 44.0 1.82 -20.5 83.2 -0.24 -76.6 112.6 0.61 -155.0 139.2 0.80 -245.9 167.0 0.87 1.025
C 41.4 37.6 1.40 51.8 67.6 1.53 59.2 92.2 1.61 60.8 105.8 1.67 67.8 121.0 1.69 1.580
D 58.4 12.0 1.17 77.6 -20.4 1.01 95.8 -61.0 0.89 105.6 -108.8 0.76 115.2 -164.0 0.63 0.892
E -46.2 17.3 0.98 -150.8 22.7 1.05 -247.4 25.1 1.07 -353.6 34.3 1.07 -465.4 38.5 1.07 1.048
Average S/N ratio for all hot spot locations 1.10
SCF/SNCF ratios for stainless steel tubular X-joint of specimen XD-C140×3-B140×3 (β=1.00, τ=1.00, 2γ=25.92)
Determination of SCF
Hot spot
location
Axial compression force (kN)
Average
S/N
ratio
16.1 32.1 47.9 64.0 79.8
ξ┴ ξ// S/N ξ┴ ξ// S/N ξ┴ ξ// S/N ξ┴ ξ// S/N ξ┴ ξ// S/N
A -160.4 26.4 1.04 -289.4 59.8 1.03 -366.8 102.8 1.01 -418.0 154.8 0.98 -456.0 213.6 0.94 1.000
B -324.6 -18.0 1.12 -709.0 -36.2 1.12 -1100.2 -49.0 1.11 -1476.6 -71.0 1.11 -1848.6 -101.6 1.12 1.116
C -207.8 -87.0 1.24 -494.2 -202.8 1.23 -809.2 -336.0 1.24 -1136.6 -476.6 1.24 -1496.6 -646.2 1.24 1.238
D -65.6 -79.8 1.50 -172.6 -187.4 1.46 -295.4 -307.6 1.44 -441.0 -437.6 1.43 -615.0 -593.6 1.42 1.450
E -4.4 23.8 -0.68 -24.0 60.2 0.27 -55.4 108.6 0.45 -99.8 162.6 0.56 -153.4 228.4 0.61 0.473
Average S/N ratio for all hot spot locations 1.06
SCF/SNCF ratios for stainless steel tubular X-joint of specimen XH-C110×4-B150×6 (β=0.77, τ=1.46, 2γ=49.32)
Determination of SCF
nSNCF /
SNCFSCF2
//
1
1
1.08
Outline
Introduction
Hot Spot Stress Method
Experimental Investigation
Finite Element Analysis
Design Guidelines
Conclusions
Finite Element Model
A
B C
D
E
F
G
H
I
Verification of FEM
Specimen Comparison
Strain concentration factor (SNCF)
A B C D E F G H I
XD-C140×3-B40×2
Experiment –– 15.03 9.52 4.39 1.27 -0.79 –– 4.26 12.27
FE model –– 15.38 8.82 3.74 0.86 -1.33 –– 4.26 9.04
SNCFEXP/SNCFFE –– 0.98 1.08 1.17 1.48 0.59 –– 1.00 1.36
XH-C150×6-B150×6
Experiment 2.11 1.91 0.91 –– 1.52 0.35 0.09 2.49 1.69
FE model 2.27 2.13 1.01 –– 2.16 0.27 0.06 1.55 1.37
SNCFEXP/SNCFFE 0.93 0.90 0.90 –– 0.70 1.30 1.50 1.61 1.23
XN-C40×4-B40×2
Experiment 1.07 0.52 0.08 -0.04 0.75 1.19 0.04 1.63 0.72
FE model 1.19 0.67 0.16 -0.03 1.20 0.74 0.04 1.14 0.65
SNCFEXP/SNCFFE 0.90 0.78 0.50 1.33 0.63 1.61 1.00 1.43 1.11
Parametric Study
Geometric parameter β=b1/b0 τ=t1/t0 2γ=b0/t0
CIDECT [0.35-1.0] [0.25-1.0] [12.5-25.0]
Laboratory tests [0.5-1.0] [0.5-1.5] [10.0-50.0]
Parametric study [0.2-1.0] [0.25-2.0] [10.0-50.0]
Outline
Introduction
Hot Spot Stress Method
Experimental Investigation
Finite Element Analysis
Design Guidelines
Conclusions
Current Design Rules hgfe
dcbaSCF
2
222
Hot spot location Coefficient
a b c d e f g h
Brace
A/E 0.013 0.693 -0.278 0 0.790 1.898 -2.109 0
Joints with fillet
welds
SCFA and SCFE are multiplied by a factor of 1.40
for brace side of weld.
Chord
B 0.143 -0.204 0.064 0 1.377 1.715 -1.103 0.75
C 0.077 -0.129 0.061 -0.0003 1.565 1.874 -1.028 0.75
D 0.208 -0.387 0.209 0 0.925 2.389 -1.881 0.75
X-joints
(β=1.0)
SCFC is multiplied by a factor of 0.65;
SCFD is multiplied by a factor of 0.50.
Comparison
Specimen β=b1/b0 τ=t1/t0 2γ=b0/t0 Comparison Stress concentration factor (SCF)
A B C D E
XD-C140×3-B40×2 0.50 0.59 24.08
Experiment 2.19 16.23 10.28 4.74 1.37
CIDECT 19.21 19.46 17.42 8.50 19.21
SCFEXP/SCFCIDECT 0.11 0.83 0.59 0.56 0.07
XD-C140×3-B140×3 1.00 1.00 25.92
Experiment 2.49 0.15 0.73 -0.55 1.39
CIDECT 3.95 1.95 2.04 1.60 3.95
SCFEXP/SCFCIDECT 0.63 0.08 0.36 -0.34 0.35
XH-C150×6-B150×6 1.00 1.02 26.17
Experiment 2.28 2.06 0.98 -0.11 1.64
CIDECT 4.01 2.08 2.00 1.64 4.01
SCFEXP/SCFCIDECT 0.57 0.99 0.49 -0.07 0.41
XH-C110×4-B150×6 0.77 1.46 49.32
Experiment 5.62 16.51 12.14 4.47 0.84
CIDECT 26.93 93.02 -12.55 28.38 26.93
SCFEXP/SCFCIDECT 0.21 0.18 -0.97 0.16 0.03
XN-C40×4-B40×2 1.00 0.52 10.55
Experiment 1.16 0.56 0.09 -0.04 0.81
CIDECT 2.31 0.19 0.68 0.27 2.31
SCFEXP/SCFCIDECT 0.50 2.95 0.13 -0.15 0.35
Proposed Design Rules
hgfedcbaSCF
2
222
Hot spot location Coefficient
a b c d e f g h
Brace
A/E/F 0.725 -2.000 2.000 -0.0025 0.270 4.350 -4.200 0.250
H 1.700 -5.000 5.000 -0.0015 -0.250 4.480 -4.200 0.500
Chord
B/I 0.191 -1.276 1.856 -0.0002 4.288 -3.800 -0.155 0.800
C 0.015 0.250 -0.250 -0.0002 1.500 0.778 -0.950 0.500
D/G 0.075 -0.300 0.540 0.0003 1.200 1.800 -2.700 0.300
Comparison
A total of 115 X-joints
Comparison
SCFFE/SCFCIDECT SCFFE/SCFProposed
A B C D A B C D H
Mean 0.80 0.99 0.17 0.54 1.00 1.00 1.00 1.00 1.00
COV 0.350 1.069 3.071 0.932 0.281 0.177 0.316 0.279 0.211
Outline
Introduction
Hot Spot Stress Method
Experimental Investigation
Finite Element Analysis
Design Guidelines
Conclusions
Conclusions
The highest SCFs are usually found for stainless steel tubular
X-joints with medium β values.
The highest SCFs may occur at the center of brace and chord
intersection edges as well as the traditional hot spot locations
for stainless steel tubular X-joints.
The lower the 2γ ratio, the lower the SCF.
Conclusions
The design rules specified in the current design guideline are
generally quite unconservative for the SCFs of cold-formed
stainless steel tubular X-joints.
The values obtained from the proposed unified design
equation for the SCFs of cold-formed stainless steel tubular X-
joints are generally much more accurate than those calculated
using the current design formulae.
The limit of the geometric parameters (β, τ and 2γ) and the
thickness of the tubular sections in the proposed unified design
equation are beyond the limit in the CIDECT design formulae.
Hefei University of Technology The University of Hong Kong
Q & A