Accession Number : ADA289320
Title : Finite Element Methods for Nonlinear Static Analysis of Sandwich Plates.
Descriptive Note : Master's thesis,
Corporate Author : AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING
Personal Author(s) : Siler, Damin J.
PDF Url : ADA289320
Report Date : DEC 1994
Pagination or Media Count : 129
Abstract : A finite element method, developed for static analysis of composite plates, was enhanced to be used with sandwich plates. The theory considers geometric nonlinearity and transverse shear. Furthermore, a new postprocessor was written to check for initial failure using the maximum stress criteria. It also includes a procedure for evaluating transverse normal stresses by enforcing equilibrium. The code modifications for sandwiches were verified by by comparing finite element solutions to closed-form sandwich theories. Both methods showed good correlation. In addition, comparisons between one type of composite plate and a similar sandwich plate found that the sandwich had better specific stiffness for various geometries. Finally, quasi-static models of low-velocity impacts on sandwich plates succeeded in predicting incipient damage due to core crushing in the impact region, but they were inconsistent in estimating the actual load levels for initial failure, based on experiments from other research.
Descriptors : *COMPOSITE STRUCTURES, *PLATES, *SANDWICH CONSTRUCTION, COMPUTER PROGRAMS, THICKNESS, STRESS ANALYSIS, LAMINATES, FINITE ELEMENT ANALYSIS, STIFFNESS, DISPLACEMENT, DEFLECTION, THESES, MESH, FORTRAN, SHEAR STRESSES, SUBROUTINES, FAILURE(MECHANICS), ASPECT RATIO.
Subject Categories : Structural Engineering and Building Technology
Distribution Statement : APPROVED FOR PUBLIC RELEASE