Accession Number : AD0608469

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

Corporate Author : BELL AEROSYSTEMS CO BUFFALO N Y

Personal Author(s) : Batt,James R.

Report Date : SEP 1964

Pagination or Media Count : 72

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)

Descriptors :   (*HYPERSONIC FLIGHT, AERODYNAMIC CHARACTERISTICS), (*AERODYNAMIC CHARACTERISTICS, HYPERSONIC FLIGHT), (*AEROTHERMOELASTICITY, FLUID DYNAMICS), AIRFOILS, LIFT, NONLINEAR SYSTEMS, STABILITY, CONTROL, PRESSURE, MATHEMATICAL ANALYSIS, MATRICES(MATHEMATICS), ANGLE OF ATTACK, WINGS

Distribution Statement : APPROVED FOR PUBLIC RELEASE