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