NONLINEAR THERMOELASTIC EFFECTS ON HYPERSONIC STABILITY AND CONTROL, PART I, VOLUME I, AERODYNAMICS,

Abstract

Linnell's pressure prediction method is used as a basis for developing hypersonic aerodynamic influence coefficient matrices. The method developed accounts for the nonlinear variation of lifting pressure with angle of attack which is present at hypersonic speeds. Comparisons of theoretical and experimental hypersonic pressure distributions are made. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1964
Accession Number
AD0608469

Entities

People

  • James R. Batt

Organizations

  • Bell Aircraft Corporation

Tags

DTIC Thesaurus Topics

  • Aerodynamics
  • Coefficients
  • Fluid Dynamics
  • Fluid Mechanics
  • Pressure Distribution

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Structural Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow