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Ultimate capacity of structural steel cross-sections under compression, bending and combined loading
Andrew Liew, Leroy Gardner Structures Volume 1, Pages 2-11 (February 2015) DOI: /j.istruc Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 1 Schematic stress–strain curves (a) for hot-rolled material, (b) cold-formed material and (c) the CSM material model. Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 2 Stub column load–deformation response.
Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 3 CSM base curve with stub column and bending test data for structural steel, stainless steel and aluminium. Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 4 Cross-section geometry for the CSM analytical bending expressions (I and box sections). Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 5 Strain distributions in cross-sections under combined axial load and bi-axial bending; compression is positive and NA is the neutral axis. Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 6 Typical interaction surface generated from the numerical model for an I-section with a strain ratio ϵcsm/ϵy=15. Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 7 Bi-axial bending interaction curves for a typical I-section at fixed axial load levels n=N/Ny. Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 8 Bi-axial bending interaction curves for a typical box section at fixed axial load levels n=N/Ny. Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 9 I-section numerical model envelopes (strain ratios 5–15) and the CSM design equation for combined loading. Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 10 Rectangular hollow section numerical model envelopes (strain ratios 3–15) and the CSM design equation for combined loading. Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 11 I-section residuals (%) between the CSM design equation and the numerical results (strain ratio of 15). Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 12 Rectangular hollow section residuals (%) between the CSM design equation and the numerical results (strain ratio of 15). Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 13 Comparison of stub column test data with EN and CSM capacity predictions. Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 14 Comparison of bending test data with EN and CSM capacity predictions. Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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Fig. 15 Comparison of test data for cross-sections under combined loading with EN (EC3) and CSM predictions. Structures 2015 1, 2-11DOI: ( /j.istruc ) Copyright © 2015 Elsevier B.V. Terms and Conditions
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