Buckling of moderately thick, laminated cylindrical shells under lateral pressure

Composites Engineering - Tập 3 Số 5 - Trang 409-417 - 1993
George J. Simitses1, Ala Tabiei1, John S. Anastasiadis1
1Department of Aerospace Engineering & Engineering Mechanics, University of Cincinnati, Cincinnati, OH 45221, U.S.A.

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Tài liệu tham khảo

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Reddy, 1990, A review of refined theories of laminated composite plates, Shock Vibr. Digest, 22, 3, 10.1177/058310249002200703

Simitses, 1976

Simitses, 1991, Buckling of axially-loaded, moderately-thick, cylindrical laminated shells, Compos. Engng, 1, 375, 10.1016/0961-9526(91)90042-Q

Simitses, 1992, Shear deformable theories for cylindrical laminates-equilibrium and buckling with applications, AIAA Jl, 30, 826, 10.2514/3.10991