Tension Buckling of Rectangular Sheets Due to Concentrated Forces
Publication: Journal of Engineering Mechanics
Volume 115, Issue 12
Abstract
Very thin rectangular plates (sheets) may buckle due to concentrated tensile forces acting upon two opposite edges. In such cases the buckling (wrinkling) mode shape has a more rapid change in the direction transverse to the loading. The plane elasticity problem is first solved to determine the internal stress field with reasonable accuracy. This is done by superimposing the exact solution for the point‐loaded circular disk upon a finite element solution for the rectangular sheet. The Ritz method is used to solve the buckling problem for all the edges simply supported. Convergence studies are made to determine the accuracies of the results. Critical buckling loads and mode shapes are determined for plates of aspect ratio 0.5, 1, and 2, loaded either at the center points or quarter points of two opposite edges by two tensile forces. The physical reality of the tension buckling phenomenon is further analyzed by calculations for the free vibration frequency spectrum of the plate. This is fhe first known theoretical study made for tension buckling of plates.
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References
1.
Alfutov, N. A., and Balabukh, L. I. (1967). “On the possibility of solving plate stability problems without a preliminary determination of the initial state of stress.” Prik. Math. Mech., 31, 730–736 (in Russian).
2.
Ayoub, E. F. (1989). “Vibration and buckling of plates subjected to inplane concentrated forces,” dissertation presented to Ohio State University, at Columbus, Ohio, in partial fulfillment of the requirements for the degree of Doctor of Philosophy.
3.
Leissa, A. W. (1973). “On a curve veering aberration.” J. Appl. Math. Phys., 25, 99–111.
4.
Leissa, A. W. (1985). “Buckling of laminated composite plates and shell panels.” Report No. AFWAL‐TR‐85‐3069, Flight Dynamics Lab., Wright‐Patterson Air Force Base, Dayton, Ohio.
5.
Leissa, A. W., and Ayoub, E. F. (1988). “Vibration and buckling of a simply supported rectangular plate subjected to a pair of inplane concentrated forces.” J. Sound Vib., 127(1), 155–171.
6.
Ritz, W. (1908). “Über eine neue Methode zur Lösung gewisser Variationsprobleme der mathematischen Physik.” J.f.d. Reine und Angew. Math., 135, 1–61 (in German).
7.
Timoshenko, S. (1910). “Stabilität einer rechteckigen Platte, die durch einzelne Kräfte gedrückt wird.” Zeit. Angew. Math. Phys., 58, 357–360 (in German).
8.
Timoshenko, S. P., and Gere, J. M. (1961). Theory of elastic stability. 2nd Ed., McGraw‐Hill Book Co., New York, N.Y.
9.
Timoshenko, S. P., and Goodier, J. N. (1970). Theory of elasticity. 3rd Ed., McGraw–Hill Book Co., New York, N.Y., 122–123.
10.
Timoshenko, S., and Woinowsky‐Krieger, S. (1959). Theory of plates and shells. 2nd Ed., McGraw‐Hill Book Co., New York, N.Y., 387.
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Copyright © 1989 ASCE.
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Published online: Dec 1, 1989
Published in print: Dec 1989
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