Accession Number : AD0608829

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

Corporate Author : BELL AEROSYSTEMS CO BUFFALO N Y

Personal Author(s) : Batt,James R.

Report Date : SEP 1964

Pagination or Media Count : 142

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)

Descriptors :   (*AEROTHERMOELASTICITY, HYPERSONIC FLOW), (*AIRFOILS, AERODYNAMIC CHARACTERISTICS), STABILITY, CONTROL, NONLINEAR SYSTEMS, GRAPHICS

Distribution Statement : APPROVED FOR PUBLIC RELEASE