Stress Analysis of Aircraft Tires. Volume 2. User's Manual

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.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1976
Accession Number
ADB021181

Entities

People

  • Alexander L. Deak

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Aircraft Tires
  • Aircrafts
  • Assembly Languages
  • Computers
  • Dynamics
  • Equations
  • Governments
  • Instructions
  • Mass Storage
  • Modulus Of Elasticity
  • Specifications
  • Stress Analysis
  • Test And Evaluation
  • Tires
  • Vehicle Equipment

Readers

  • Computer Science.
  • Structural Dynamics.