Accession Number : AD0747408

Title :   A Circular Cone under an Angle of Attack in a Supersonic Flow of Gas,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Sapunkov,Ya. G.

Report Date : 26 MAY 1972

Pagination or Media Count : 17

Abstract : An investigation is reported of the flow around a cone at a small angle of attack by a uniform supersonic flow of an ideal gas. The problem is solved by the method of small disturbances. The present work presents a solution in the eddy layer with favorable accuracy. The desired solution is reduced in the work to quadratures. (Author)

Descriptors :   (*CONICAL BODIES, *SUPERSONIC CHARACTERISTICS), GAS FLOW, ANGLE OF ATTACK, MATHEMATICAL ANALYSIS, FLOW FIELDS, THEORY, VORTICES, USSR

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE