2016
DOI: 10.1515/ama-2016-0033
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Local and Distortional Buckling of Axially Loaded Cold Rolled Sigma Profiles

Abstract: In this paper the local and distortional buckling analyses of axially loaded cold-rolled channel and sigma profiles were performed. The critical buckling load was computed by solving the linear eigenvalue problem for different numerical models using Finite Element Method and simplified formulas implemented in Eurocode and proposed by Hancock and Schafer. The buckling analyses were conducted to prove that the sigma cross-section can be successfully replaced by channel cross-section with additional elastic suppo… Show more

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Cited by 2 publications
(3 citation statements)
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“…However, in many technically important cases this model is too conservative, which has been confirmed by numerous experimental studies, e.g., References [5,[12][13][14]; theoretical studies, e.g., References [4,7,15,16]; and numerical simulations, e.g., References [17][18][19][20][21][22][23]. This is due to the fact that in real thin-wall cross-sections, there is an effect of mutual, elastic interaction of component plates (walls).…”
Section: Computational Model For Local Cross-section Bucklingmentioning
confidence: 99%
“…However, in many technically important cases this model is too conservative, which has been confirmed by numerous experimental studies, e.g., References [5,[12][13][14]; theoretical studies, e.g., References [4,7,15,16]; and numerical simulations, e.g., References [17][18][19][20][21][22][23]. This is due to the fact that in real thin-wall cross-sections, there is an effect of mutual, elastic interaction of component plates (walls).…”
Section: Computational Model For Local Cross-section Bucklingmentioning
confidence: 99%
“…The buckling analyses of cold-formed steel sigma cross-sections in purlin-sheeting systems subjected to uniformly distributed uplift load were conducted in [12]. Axially loaded cold-formed sigma profi les were investigated in order to defi ne their local and distortional buckling behaviour [13].…”
Section: Introductionmentioning
confidence: 99%
“…The formula (13) can also be presented as: (14) where: V z -shear force in "z" axis direction, S ymoment of stability in respect to "y" axis, I y -moment of inertia in respect to "y" axis, V y -shear force in "y" axis direction, S z -moment of stability in respect to "z" axis, I z -moment of inertia in respect to "z" axis, M ω -warping-torsional moment, S ω -sectional static moment, I ω -a sectional moment of inertia, M T -torsional moment, I T -a torsional moment of inertia, t -wall thickness.…”
Section: Introductionmentioning
confidence: 99%