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Longitudinal stiffeners for compression members
Simplified methods based on buckling strength are developed for proportioning stiffening lips on thin flanges and intermediate stiffeners on thin sheet subjected to uniform compression; symmetrical and unsymmetrical stiffeners and lips are considered; buckling strengths are determined from equivalent slenderness ratio formulas presented and column buckling equations; radius of gyration of stiffener or lip required to provide essentially hinge support for flange or sheet at stiffener is developed; compression tests of thin-gage hat sections of aluminum alloy 6061-T6 provide information on buckling strength and behavior of sections with lipped flanges.
Longitudinal stiffeners for compression members
Simplified methods based on buckling strength are developed for proportioning stiffening lips on thin flanges and intermediate stiffeners on thin sheet subjected to uniform compression; symmetrical and unsymmetrical stiffeners and lips are considered; buckling strengths are determined from equivalent slenderness ratio formulas presented and column buckling equations; radius of gyration of stiffener or lip required to provide essentially hinge support for flange or sheet at stiffener is developed; compression tests of thin-gage hat sections of aluminum alloy 6061-T6 provide information on buckling strength and behavior of sections with lipped flanges.
Longitudinal stiffeners for compression members
ASCE -- Proc (J Structural Div)
Sharp, M.L. (author)
1966
25 pages
Article (Journal)
English
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