NONLINEAR THERMOELASTIC EFFECTS ON HYPERSONIC STABILITY AND CONTROL. PART II. ANALYTICAL AND EXPERIMENTAL STATIC AEROTHERMOELASTICITY,

Abstract

An analytical method was developed for the analysis of static aerothermoelastic behavior in the presence of nonlinear aerodynamic loads and geometrically nonlinear structural behavior. The method was programmed for the IBM 7090 digital computer using FORTRAN coding techniques. A system for the experimental determination of static aerothermoelastic response of nonuniformly heated structures to loadings which are a nonlinear function of wing surface slopes was developed. Results of this experimental program are presented and compared with theoretical predictions. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1964
Accession Number
AD0608476

Entities

People

  • James R. Batt
  • Richard H. Gallagher

Organizations

  • Bell Aircraft Corporation

Tags

DTIC Thesaurus Topics

  • Aerothermoelasticity
  • Computer Programming
  • Computers
  • Computing Devices
  • Computing-Related Activities
  • Digital Computers
  • Software Development

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Structural Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow