THERMAL STRESS DETERMINATION TECHNIQUES FOR SUPERSONIC TRANSPORT AIRCRAFT STRUCTURES

Abstract

This report describes computer programs developed for the analysis of heated beams, plates, and stiffened cylindrical shells. The matrix displacement approach to structural analysis, which forms the theoretical basis of these programs, is developed in detail. Derivation of new relationships employed in these programs is also detailed. The capabilities and limitations of the respective programs are outlined and illustrative applications are presented.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1964
Accession Number
AD0432024

Entities

People

  • J. Padlog
  • R. D. Huff
  • R. H. Gallagher

Organizations

  • Bell Aircraft Corporation

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Climate Change
  • Computer Programs
  • Computers
  • Creep
  • Fuselages
  • Geometry
  • Mechanical Working
  • Modulus Of Elasticity
  • Stiffness
  • Stress Analysis
  • Stress Strain Relations
  • Stresses
  • Structural Analysis
  • Supersonic Transport Aircraft
  • Temperature Gradients
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Structural Dynamics.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics