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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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1949.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1971. |
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| 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. |
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| Item Description: | "October 1949." NACA TN Number 1971. |
| Physical Description: | 15 pages : illustrations ; 28 cm. |
| Bibliography: | Includes bibliographical references. |