By W. T. Koiter (auth.), Professor Bernard Budiansky (eds.)
This quantity includes the written texts of the papers offered at a Symposium on Buckling of buildings held at Harvard college in June 1974. This symposium, among the many on numerous subject matters backed each year by way of the overseas Union of Theoretical and utilized Me chanics (IUTAM), used to be prepared by means of a systematic Committee inclusive of B. Budiansky (Chairman), A. H. Chilver, W. T. Koiter, and A. S. Vol' mir. Participation was once by means of invitation of the clinical Committee, and particular academics have been invited to talk within the parts of experimental examine, buckling and post-buckling calculations, post-buckling mode interplay, plasticity and creep results, dynamic buckling, stochastic difficulties, and layout. a complete of 29 lectures have been introduced, together with a basic beginning lecture through Professor Koiter, and there have been ninety three reg istered members from sixteen various nations. monetary help for the symposium was once supplied by means of IUTAM, within the type of partial commute help for a few members, and likewise through the nationwide technology beginning, the nationwide Aeronautics and house management, and the Air strength workplace of clinical Re seek, for added go back and forth aid and administrative expenditures. assembly amenities and prone have been successfully supplied through the technological know-how middle of Harvard college, and administrative help was once gen erously supplied through the department of Engineering and utilized Physics of Harvard collage. The medical chairman loved the important counsel of his colleagues Professors J. W. Hutchinson and J. L.
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Extra info for Buckling of Structures: Symposium Cambridge/USA, June 17–21, 1974
Williams, F. : Computation of Natural Frequencies and Initial Buckling Stresses of Prismatic Plate Assemblies. J. of Sound and Vibration 21,87 -106 (1972). 7. Williams, F. ; Wittrick, W. : Numerical Results for the Initial Buckling of Some Stiffened Panels in Compression. Aeronautical Quarterly XXIII, 24-40 (1972). 8. Plank, R. ; Williams, F. : Critical Buckling of Some Stiffened Panels in Compression, Shear and Bending. Aeronautical Quarterly XXV, 165-179 (1974). 9. Williams, F. : Stiffened Panels with Varying Stiffener Sizes.
Effect of Higher Order Terms in Certain Nonlinear Finite Element Models. AIAA J. 11,1589-1590 (1973). 21. Gallagher, R. : Finite Element Analysis of Geometrically Nonlinear Problems. In: Theory and Practice in Finite Element Structural Analysis. Y. Yamada and R. , Univ. of Tokyo Press 1973, pp. 109-123. 22. ; Haisler, W. : Survey of Solution Procedures for Nonlinear Static and Dynamic Analyses. Proc. of SAE Internat. Conf. on Vehicle Structural Mechanics. Detroit: Mich. Mar. 1974, pp. 1-17. 23_ Zienkiewicz, O.
Aeronautical Quarterly XXV, 165-179 (1974). 9. Williams, F. : Stiffened Panels with Varying Stiffener Sizes. J. of the Royal Aeronautical Society 77, 350-354 (1973). 10. Wittrick, W. : General Sinusoidal Stiffness Matrices for Buckling and Vibration Analyses of Thin Flat-Walled Structures. Int. J. of Mech. Sci. 10, 949-966 (1968) 11. Williams, F. : Approximations in Complicated Critical Buckling and Free Vibration Analyses of Prismatic Plate Structures. Aeronautical Quarterly XXV, 180-185 (1974).