Inclusion of transverse shear deformation in exact buckling and vibration analysis of composite plate assembliesThe problem considered is the development of the necessary plate stiffnesses for use in a general purpose program for buckling and vibration of composite plate assemblies. The required stiffnesses are for the assumption of sinusoidal response along the plate length with transverse shear included. The method is based on the exact solution of the plate differential equations for a composite laminate having fully populated A, B, and D matrices which leads to a differential equation of tenth order.
Document ID
19920051681
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, Melvin S. (Old Dominion University Research Foundation, Norfolk, VA, United States)
Kennedy, David (Cardiff, University College, United Kingdom)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 92-2287
Meeting Information
Meeting: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference