Accession Number : AD0763283

Title :   Shock Wave Incidence on a Wedge Moving at Supersonic Speed,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Arutyunyan,G. M.

Report Date : 06 JUN 1973

Pagination or Media Count : 12

Abstract : A flow which is developing at the upper surface of a wedge moving at supersonic speed, when a plane shock wave is incident on the wedge, can be calculated in the framework of a linearized theory, if the point which is determined by two parameters of the wedge belongs to a certain area in the reference plane.

Descriptors :   (*WEDGES, *SUPERSONIC CHARACTERISTICS), (*SHOCK WAVES, INTERACTIONS), THEORY, MATHEMATICAL MODELS, ANGLE OF ATTACK, SURFACE PROPERTIES, FLOW FIELDS, USSR

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE