Buckling and Postbuckling of Composite Plates by A. W. Leissa (auth.), G. J. Turvey, I. H. Marshall (eds.)

By A. W. Leissa (auth.), G. J. Turvey, I. H. Marshall (eds.)

Contributed by means of prime professionals within the box from around the globe, this article offers a complete perception into buckling and postbuckling. simple concept, tools of buckling research and their software, the influence of exterior variables reminiscent of temperature and humidity at the buckling reaction and buckling checks are all covered.

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Whitney, J. M. (1987) Structural Analysis of Laminated Composite Plates, Technomic Publishing, Lancaster, PA. 10. Leissa, A. W. (1973) Vibration of Shells, NASA SP-288, US Govt. Printing Office, Washington, DC. 11. Narita, Y. and Leissa, A. W. (1990) Buckling studies for simply supported symmetrically laminated rectangular plates. International Journal of Mechanical Sciences, 32 (11), 309-24. 12. Leissa, A. W. (1969) Vibration of Plates, NASA SP-160, US Govt. Printing Office, Washington, DC. 13.

21). 58) It is observed that the left-hand side of equation (1. 56) consists of linear terms as in the classical bifurcation buckling problem, and that the righthand side contains only non-linear terms which arise from the in-plane stresses caused by the postbuckling deformation. g. unsymmetrical) composite plate, with transverse shear deformation neglected. Certain simplifications are possible for symmetrical laminates. g. 57). g. cross-ply) then, in addition, A]6=A26=D]6=D26=0. Detailed simplified forms are given by Chia [23].

2, taken from Ref. [IS], where results are presented for singlelayer (8 = 30°) and three-layer (8 = 30", - 30=,30°) square plates subjected to five types of loading conditions, Cases (l)-(S). 4Sa-e). 2, results are given for four sizes of solution: M x N (number of terms used in the X and Y directions, respectively) = 6 x 6,8 x 8,10 x 10 and 12 x 12. These solutions result in eigenvalue determinants of order 36,64,100 and 144, respectively. 5% in Au is observed relative to the 12 x 12 solution for graphite/ epoxy single-layer plates.

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