Accession Number : AD0625404

Title :   CALCULATION OF THE FORCE COEFFICIENT FOR DELTA WINGS IN HYPERSONIC FLOW.

Descriptive Note : Interim rept. Apr 64-Jun 65,

Corporate Author : CINCINNATI UNIV OHIO HYPERSONIC AERODYNAMICS RESEARCH STAFF

Personal Author(s) : Polak,Arnold

Report Date : SEP 1965

Pagination or Media Count : 43

Abstract : The results of the Newtonian theory as applied to a delta wing at moderate angles of attack in hypersonic stream are used to calculate the pressure coefficient by the inverse method in a closed form. (Author)

Descriptors :   (*DELTA WINGS, AERODYNAMIC LOADING), (*HYPERSONIC CHARACTERISTICS, DELTA WINGS), MATHEMATICAL ANALYSIS, BOUNDARY LAYER, ASPECT RATIO, PRESSURE, HYPERSONIC FLOW

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE