Design of antisymmetric hybrid laminates for maximum buckling load: I. Optimal fibre orientation
- 31 December 1990
- journal article
- Published by Elsevier in Composite Structures
- Vol. 14 (1) , 49-60
- https://doi.org/10.1016/0263-8223(90)90058-m
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Optimal fibre orientation for simply-supported, angle-ply plates under biaxial compressionComposite Structures, 1988
- A review of the tensile, compressive, flexural and shear properties of hybrid fibre-reinforced plasticsComposites, 1987
- Deflection analysis of hybrid laminated composite platesComposite Structures, 1986
- Transverse vibrations of hybrid laminated platesJournal of Sound and Vibration, 1986
- Optimal Design of Laminated Composite Plates Under Axial CompressionTransactions of the Canadian Society for Mechanical Engineering, 1985
- Multiobjective Design of an Antisymmetric Angle-Ply Laminate by Nonlinear ProgrammingJournal of Mechanical Design, 1983
- Optimum Design of Laminated Plates under Axial CompressionAIAA Journal, 1979
- Minimizing the mass of reinforced rectangular plates compressed in two directions in a manner conducive toward stabilityMechanics of Composite Materials, 1977
- Optimization of Buckling and Yield Strengths of Laminated CompositesAIAA Journal, 1975