Journal of Aerospace System Engineering (항공우주시스템공학회지)
- Volume 1 Issue 4
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- Pages.28-36
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- 2007
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- 1976-6300(pISSN)
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- 2508-7150(eISSN)
Critical Buckling Loads of Laminated Composites under Cylindrical Bending
원통형 굽힘을 받는 적층판의 임계좌굴 하중
Abstract
This paper presents critical buckling loads of laminated composites under cylindrical bending. In-plane displacements are assumed to vary exponentially through plate thickness. The accuracy of this theory is examined for symmetric/antisymmetric cross-ply, angle-ply and unsymmetric laminates under cylindrical bending. Analytical solutions are provided to investigate the effect of transverse shear deformation on critical buckling loads of the laminated plates, and the results are compared with those obtained from the first-order shear deformation plate theory and the classical laminated plate theory.