Storming Media: Pentagon Reports and DocumentsPentagon Reports: Fast. Definitive. Complete.     
New Account »
Forgot Password?
Advanced Search »

Materials SciencesLaminates and Composite Materials

A Finite-Difference Program for Stresses in Anisotropic, Layered Plates in Bending

Authors: Nicholas J. Salamon; NATIONAL AERONAUTICS AND SPACE ADMINISTRATION HUNTSVILLE AL GEORGE C MARSHALL SPACE FLIGHT CENTER
 
Abstract: Results from the initial phase of a study of the interlaminar stresses induced in a layered laminate that is bent into a cylindrical surface are given. The laminate is modeled as a continuum, and the resulting elasticity equations are solved using the finite-difference method. The report sets forth the mathematical framework, presents some preliminary results, and provides a listing and explanation of the computer program. Significant among the results are apparent symmetry relationships that will reduce the numerical size of certain problems and an interlaminar stress behavior having a sharp rise at the free edges.

Limitations: APPROVED FOR PUBLIC RELEASE DOCUMENT PARTIALLY ILLEGIBLE
Description: Technical note
Pages: 89
Report Date: SEP 75
Report Number: A270503
Keywords relating to this report:
*LAMINATES
*STRESS ANALYSIS
BENDING STRESS
COMPUTER PROGRAMS
DISPLACEMENT
ELASTIC PROPERTIES
FINITE DIFFERENCE THEORY
GRAPHITE EPOXY COMPOSITES
LOAD DISTRIBUTION
LOADS_FORCES_
MATHEMATICAL MODELS
MATRICES_MATHEMATICS_
PARTIAL DIFFERENTIAL EQUATIONS
PHASE STUDIES
SHEAR STRESSES
STRESS CONCENTRATION
STRESS STRAIN RELATIONS
SYMMETRY
Adobe PDF - $21.95
Printed Format - $24.95
Please check the box for the format you wish to order.
Shipping Terms
About Electronic Delivery

Email This Abstract