Download e-book for kindle: A Unified theory of plastic buckling of columns and plates by Elbridge Z Stowell

By Elbridge Z Stowell

ISBN-10: 1680156373

ISBN-13: 9781680156379

At the foundation of recent plasticity issues, a unified conception of plastic buckling acceptable to either columns and plates has been built. For uniform compression, the speculation exhibits exhibits that lengthy columns which bend with out considerable twisting require the tangent modulus and that lengthy flanges which twist with no considerable bending require the secant modulus. constructions that either bend and twist whilst they Read more...

summary: at the foundation of contemporary plasticity concerns, a unified idea of plastic buckling appropriate to either columns and plates has been constructed. For uniform compression, the speculation exhibits exhibits that lengthy columns which bend with out considerable twisting require the tangent modulus and that lengthy flanges which twist with no considerable bending require the secant modulus. constructions that either bend and twist after they buckle require a modulus that's a mix of the secant modulus and the tangent modulus

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Extra resources for A Unified theory of plastic buckling of columns and plates

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V61,’14, no. 5, w 1947, PP: 262-567. 13, .. ~ Secant Modulus Methotl”forDetermining Plate ,’-~n&tab~li%yabove the Proportional Limit. Jour. Aero. , vol. 13,no. 1$ Jem. i Dete~ination of’Plate Compressive Stre@hs. ‘! ,. 1480, X347 ,’ * , . 7. Handelmen, F. : Plastic Bu&lfng of a Recta&ular Plate under Edge Thrusts. 1530, 1948, A 8. Ilyushin, A. : The Elast@Plastic Stability of Plates. 1188, 1947. 9. Compressive Stress for Outstanding Flanges. NACA Rep. No. 734, 1942. : Critical Compressive Stress for Flat Rectangular Plates Supported along All Edges and Elastically Restrained against Rotation along the Unloaded Edges.

Arado~. no. Dec. 1946, p. 678. Jo&. Aero. ~ vol. a&ticColumn Thec~*y, Jour. Aero. , V61,’14, no. 5, w 1947, PP: 262-567. 13, .. ~ Secant Modulus Methotl”forDetermining Plate ,’-~n&tab~li%yabove the Proportional Limit. Jour. Aero. , vol. 13,no. 1$ Jem. i Dete~ination of’Plate Compressive Stre@hs. ‘! ,. 1480, X347 ,’ * , . 7. Handelmen, F. : Plastic Bu&lfng of a Recta&ular Plate under Edge Thrusts. 1530, 1948, A 8. Ilyushin, A. : The Elast@Plastic Stability of Plates. 1188, 1947. 9. Compressive Stress for Outstanding Flanges.

Jour. Aero. , vol. 13,no. 1$ Jem. i Dete~ination of’Plate Compressive Stre@hs. ‘! ,. 1480, X347 ,’ * , . 7. Handelmen, F. : Plastic Bu&lfng of a Recta&ular Plate under Edge Thrusts. 1530, 1948, A 8. Ilyushin, A. : The Elast@Plastic Stability of Plates. 1188, 1947. 9. Compressive Stress for Outstanding Flanges. NACA Rep. No. 734, 1942. : Critical Compressive Stress for Flat Rectangular Plates Supported along All Edges and Elastically Restrained against Rotation along the Unloaded Edges. NACA Rep, No.

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A Unified theory of plastic buckling of columns and plates by Elbridge Z Stowell


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