Accession Number : AD0715280
Title : Bending, Vibrations, and Buckling of Laminated Anisotropic Rectangular Plates.
Descriptive Note : Technical rept. Apr 69-Jan 70,
Corporate Author : AIR FORCE MATERIALS LAB WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Whitney,James M.
Report Date : AUG 1970
Pagination or Media Count : 35
Abstract : Solutions are obtained for the bending, vibrations, and buckling of two special cases of laminated anisotropic rectangular plates displying bending-extendional coupling. Three sets of boundary conditions for simply-supported plates are considered. Plates clamped along two opposite sides and simply-supported along the two adjacent sides are also treated. Bending deflections, fundamental vibration frequencies, and buckling loads for certain orientations of angle-ply fiber reinforced composites are shown to be significantly affected by different clamped boundary conditions. Numerical results also show the effects of bending-entensional coupling can be severe for all the boundary conditions considered. (Author-PL)
Descriptors : (*STRUCTURAL MEMBERS, BUCKLING), (*AEROSPACE CRAFT, *COMPOSITE MATERIALS), LAMINATES, VIBRATION, BENDING, NUMERICAL ANALYSIS
Subject Categories : Laminates and Composite Materials
Distribution Statement : APPROVED FOR PUBLIC RELEASE