Plastic buckling of extruded composite sections in compression / Elbridge Z. Stowell and Richard A. Pride.

The theory of plastic buckling, originally developed for individual plates, has been extended to apply to combinations of plates such as H- and Z-sections. The theory has been applied specifically to extruded H-sections of 75S-T aluminum alloy; the calculated buckling stresses agree satisfactorily w...

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Bibliographic Details
Main Author: Stowell, Elbridge Z.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Pride, Richard A.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1949.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 1971.
Subjects:
Description
Summary:The theory of plastic buckling, originally developed for individual plates, has been extended to apply to combinations of plates such as H- and Z-sections. The theory has been applied specifically to extruded H-sections of 75S-T aluminum alloy; the calculated buckling stresses agree satisfactorily with the results of tests.
Item Description:"October 1949."
NACA TN Number 1971.
Physical Description:15 pages : illustrations ; 28 cm.
Bibliography:Includes bibliographical references.