Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part I, Volume 2, Aerodynamics

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Report Number: FDL TDR 64-16 Part 1 Volume 2
Author(s): Batt, James R.
Corporate Author(s): Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Pages: 142
Contract: AF 33(657)-7486
DoD Project: 8219
DoD Task: 821901
Identifier: AD0608829

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.

Provenance: Lockheed Martin Missiles & Fire Control

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