Accession Number : ADA116439
Title : Free-Edge and Contact-Edge Singularities in Laminated Composites.
Descriptive Note : Final rept. 15 Aug 80-15 Aug 81,
Corporate Author : ILLINOIS UNIV AT CHICAGO CIRCLE DEPT OF MATERIALS ENGINEERING
Personal Author(s) : Zwiers,R I ; Ting,T C T
PDF Url : ADA116439
Report Date : Apr 1982
Pagination or Media Count : 88
Abstract : This effort is part of the predictive response capability development to provide design criteria for space vehicles. For example, mechanical joints in structure have stress risers around the bolt holes due to the singularities from linear analysis. In this task the stress singularities at the free-edge and at the contact-edge of an interface in a laminated composite are studied. The composite is subjected to a uniform extension in the direction parallel to the plane of laminate layers.
Descriptors : *Composite materials, *Laminates, *Stress concentration, *Mechanical components, *Mathematical analysis, Matrices(Mathematics), Elastic properties, Eigenvalues, Anisotropy, Complex variables, Interfaces, Layers, Edges, Homogeneity, Spacecraft, Fastenings, Joints, Bolts, Holes(Openings), Numerical methods and procedures, Test and evaluation
Subject Categories : Laminates and Composite Materials
Distribution Statement : APPROVED FOR PUBLIC RELEASE