Accession Number : ADA193165
Title : Physical Mechanisms in Shock-Induced Turbulent Separated Flow.
Descriptive Note : Annual rept. 1 Mar 86-30 Nov 87,
Corporate Author : TEXAS UNIV AT AUSTIN DEPT OF AEROSPACE ENGINEERING AND ENGINEERING MECHANICS
Personal Author(s) : Dolling, D S
PDF Url : ADA193165
Report Date : 15 Dec 1987
Pagination or Media Count : 45
Abstract : It has been demonstrated that the flow downstream of the moving shock is separated and that the foot of the shock is effectively the instantaneous separation point. The shock induced turbulent separation is an intermittant process and the separation line indicated by surface tracer methods, such as kerosene-lampblack, is a downstream boundary of a region of intermittent separation. Keywords: Shock induced separation, Turbulent boundary layers, Reattachment.
Descriptors : *SHOCK, *TURBULENT BOUNDARY LAYER, *FLOW SEPARATION, BOUNDARIES, DOWNSTREAM FLOW, MOTION, PHYSICAL PROPERTIES, REGIONS, TURBULENCE, ATTACHMENT
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE