Accession Number : ADB021181
Title : Stress Analysis of Aircraft Tires. Volume II. User's Manual.
Descriptive Note : Final rept. 24 Jun 74-8 Jan 76,
Corporate Author : MATHEMATICAL SCIENCES NORTHWEST INC BELLEVUE WA
Personal Author(s) : Deak, Alexander L.
Report Date : FEB 1976
Pagination or Media Count : 40
Abstract : Presented is the nonlinear finite element analysis of multi-layered aircraft tires. A piecewise parabolic shear stress distribution is introduced to cope with arbitrary stress distribution across the thickness coordinate. Each layer is an orthotropic ply consisting of cords embedded in an elastic rubber matrix. Triangular plate elements are used with five generalized displacements at the nodes. The computer code is written for the CDC-6600 machine under the Scope 3.3 and 3.4.3 operating systems. (Author)
Descriptors : *AIRCRAFT TIRES, *STRESS ANALYSIS, *COMPUTER PROGRAMS, INFLATING, LOADS(FORCES), ROTATION, MEMORY DEVICES, ALLOCATIONS, INPUT OUTPUT PROCESSING, FINITE ELEMENT ANALYSIS, COMPUTATIONS, STIFFNESS, MATRICES(MATHEMATICS), ASSEMBLY LANGUAGES, SUBROUTINES, LAMINATES, LAYERS, MANUALS, USER NEEDS.
Subject Categories : Aircraft
Computer Programming and Software
Distribution Statement : APPROVED FOR PUBLIC RELEASE