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Frontiers of Structural and Civil Engineering

ISSN 2095-2430

ISSN 2095-2449(Online)

CN 10-1023/X

Postal Subscription Code 80-968

2018 Impact Factor: 1.272

Front. Struct. Civ. Eng.    2022, Vol. 16 Issue (4) : 461-477    https://doi.org/10.1007/s11709-022-0818-0
RESEARCH ARTICLE
Degree of bending of concrete-filled rectangular hollow section K-joints under balanced-axial loadings
Rui ZHAO1, Yongjian LIU1,2(), Lei JIANG1,2, Yisheng FU1, Yadong ZHAO1, Xindong ZHAO1
1. School of Highway, Chang’an University, Xi’an 710064, China
2. Research Center of Highway Large Structure Engineering on Safety of Ministry of Education, Xi’an 710064, China
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Abstract

It has been found that the fatigue life of tubular joints is not only determined by the hot spot stress, but also by the stress distribution through the tube thickness represented as the degree of bending (DoB). Consequently, the DoB value should be determined to improve the accuracy of fatigue assessment for both stress-life curve and fracture mechanics methods. Currently, no DoB parametric formula is available for concrete-filled rectangular hollow section (CFRHS) K-joints, despite their wide use in bridge engineering. Therefore, a robust finite element (FE) analysis was carried out to calculate the DoB of CFRHS K-joints under balanced-axial loading. The FE model was developed and verified against a test result to ensure accuracy. A comprehensive parametric study including 190 models, was conducted to establish the relationships between the DoBs and four specific variables. Based on the numerical results, design equations to predict DoBs for CFRHS K-joints were proposed through multiple regression analysis. A reduction of 37.17% was discovered in the DoB, resulting in a decrease of 66.85% in the fatigue life. Inclusively, the CFRHS K-joints with same hot spot stresses, may have completely different fatigue lives due to the different DoBs.

Keywords fatigue assessment      K-joint      design equations      degree of bending      fracture mechanics     
Corresponding Author(s): Yongjian LIU   
Just Accepted Date: 15 April 2022   Online First Date: 27 June 2022    Issue Date: 09 August 2022
 Cite this article:   
Rui ZHAO,Yongjian LIU,Lei JIANG, et al. Degree of bending of concrete-filled rectangular hollow section K-joints under balanced-axial loadings[J]. Front. Struct. Civ. Eng., 2022, 16(4): 461-477.
 URL:  
https://academic.hep.com.cn/fsce/EN/10.1007/s11709-022-0818-0
https://academic.hep.com.cn/fsce/EN/Y2022/V16/I4/461
Fig.1  Stress distribution through the chord wall thickness at weld toe.
Fig.2  Geometric parameters of the CFRHS K-joint.
steel plate thickness (mm)elastic modulus ES (GPa)yield strength fy (MPa)ultimate strength fu (MPa)elongation (%)
420642558928.0
620641457529.0
820644559328.5
Tab.1  Steel material properties
concrete grademix ratio (kg/m3)elastic modulus Ec (GPa)cube crushing strength fcu (MPa)
watercementfly ashfine aggregatecoarse aggregatewater reducer
C5016747152624110910.463056.3
Tab.2  Concrete mix ratio and material properties
parameterdetail A Ψ = 180° – 135°detail B ψ = 150° – 50°detail C ψ = 75° – 30°detail D ψ = 40° – 15°
joint-included angle (α)
 max90°Ψ ≤ 105°:60°40°; 60° for ψ is big
 min45°37.5°; 1/2ψ for ψ is small1/2ψ
bevel angle of brace (ω)
 max90°determined based on the α
 min10; 45° for Ψ > 105°10°
complete weld
  hetbtb for Ψ ≥ 90°; ?tbsinψ for Ψ < 90°?tbsinψ but ≤ 1.75 tb≥2tb
  hL?tbsinψ but ≤ 1.75 tb
Tab.3  Details of the weld profile according to the GB 50661-2011 Chinese specification
Fig.3  Details of the weld profile in the GB 50661-2011 Chinese specification. (a) Stepped joints; (b) full-width joints; (c) welding details.
Fig.4  Finite element model.
number of layers of elements through the tube thicknessDoB
10.8271
20.8448
30.8516
40.8581
50.8590
60.8592
Tab.4  Mesh sensitivity analysis for a typical joint (β = 0.7, 2γ = 30, τ = 0.75, θ = 30°)
Fig.5  Density of different meshes through the tube thickness. (a) 1 layer; (b) 2 layers; (c) 3 layers; (d) 4 layers; (e) 5 layers; (f) 6 layers.
Fig.6  Boundary and loading conditions.
distance from weld toechordbrace
Lmin0.4t0 but ≥ 4 mm0.4t1 but ≥ 4 mm
LmaxLmin + t0Lmin + t1
Tab.5  The extrapolated region as recommended by IIW-XV-E
Fig.7  Extraction of the hot spot stress.
Fig.8  Geometry of specimen and arrangement of strain gauges (unite: mm). (a) General arrangement of truss girder; (b) test joint diagram; (c) measuring-point arrangement of HSS.
Fig.9  Test setup. (a) General arrangement of experiment; (b) local arrangement of experiment.
Fig.10  FE modeling and verification. (a) FE model of the truss; (b) comparison of Load-Displacement curve between FE results and test results; (c) comparison of HSS between FE results and test results.
parametervalues
β0.4, 0.55, 0.7, 0.85, 1
2γ10, 15, 20, 25, 30, 35
τ0.25, 0.5, 0.75, 1
θ30°, 45°, 60°
Tab.6  Specific parameters for parametric analysis
Fig.11  The HSS distribution (β = 0.4, 2γ = 10, τ = 0.75, θ = 45°).
Fig.12  Influence of four variables on hot spot location (a) β; (b) 2γ; (c) τ; (d) θ.
Fig.13  A comparison of the DOBCFRHS and DOBCHS (β = 0.4, 2γ = 10, τ = 0.75, θ = 45°). (a) CFRHS K-joint; (b) RHS K-joint.
Fig.14  Influence of β on the DoB under balanced axial force (τ = 0.25, θ = 30°).
Fig.15  Influence of γ on the DoB under balanced axial force (β = 0.7, θ = 45°).
Fig.16  Influence of τ on the DoB under balanced axial force (2γ = 30, θ = 30°).
Fig.17  Influence of θ on the DoB under balanced axial force (β = 0.4, τ = 1).
Fig.18  Error analysis of the DoBs.
Fig.19  A comparison of SCFCFRHS and SCFCHS.
Fig.20  A comparison of DoBCFRHS and DoBCHS.
Fig.21  Remaining life prediction process for CFRHS K-joints based on fracture mechanics.
input parametersjoint
joint 1joint 2
chord length L03000 mm3000 mm
chord width b0400 mm400 mm
chord height h0400 mm400 mm
chord thickness t027 mm13 mm
brace length L11500 mm1500 mm
brace width b1160 mm340 mm
brace height h1160 mm340 mm
brace thickness t113 mm3 mm
brace inclination θ30°30°
axial load10000N10000N
fracture toughness63 N·mm?3/263 mm?3/2
crack growth equationParisParis
C5.21×10?13 mm?3/25.21×10?13 mm?3/2
m33
initial crack depth ai0.1 mm0.1 mm
initial crack length 2c55
final crack depth af0.99t00.99t0
Tab.7  Input parameters used for remaining fatigue life prediction of CFRHS K-joints
jointSCFDoBfatigue life (×104)
12.080.78236.8
22.050.4978.5
Tab.8  Remaining fatigue life prediction of CFRHS K-joints
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