Accession Number:

AD0608829

Title:

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

Descriptive Note:

Corporate Author:

BELL AEROSYSTEMS CO BUFFALO N Y

Personal Author(s):

Report Date:

1964-09-01

Pagination or Media Count:

142.0

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

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE