NONLINEAR THERMOELASTIC EFFECTS ON HYPERSONIC STABILITY AND CONTROL. PART I, VOLUME 2. AERODYNAMICS,

Abstract

The curves presented in this volume of the final report are to be used to obtain aerodynamic influence coefficient matrices for slender two-dimensional airfoils in hypersonic inviscid flow. Influence coefficients are presented for ten airfoil shapes as a function of thickness ratio, Mach number and geometric angle of attack. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1964
Accession Number
AD0608829

Entities

People

  • James R. Batt

Organizations

  • Bell Aircraft Corporation

Tags

DTIC Thesaurus Topics

  • Aerodynamics
  • Coefficients
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Geometry
  • Inviscid Flow
  • Mach Number
  • Mathematics
  • Physical Properties
  • Thickness
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Structural Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow