Accession Number : AD0675441

Title :   HYPERSONIC FLOW AROUND A TRIANGULAR PLATE WITH BLUNTED LEADING EDGES,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Lunev,V. V.

Report Date : 05 JAN 1968

Pagination or Media Count : 14

Abstract : Hypersonic flow of a perfect gas with a constant adiabatic exponent past a triangular plate with a 20 degree apex angle and blunted leading edges at zero angle of attack is discussed. The simplest two-layer flow pattern is used in analysis to obtain qualitative results, giving a clear picture of interrelations among the flow parameters. (Author)

Descriptors :   (*BLUNT BODIES, HYPERSONIC CHARACTERISTICS), FLOW FIELDS, MATHEMATICAL ANALYSIS, FLAT PLATE MODELS, ENTROPY, BOUNDARY LAYER, LEADING EDGES, ANGLE OF ATTACK, PRESSURE, DENSITY, EQUATIONS OF MOTION, USSR, TWO DIMENSIONAL FLOW

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE