Accession Number : AD0276874

Title :   THE EFFECT OF VISCOSITY ON THE FLOW IN THE REGION OF A STRAIGHT COMPRESSION SHOCK

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : ZUBKOV,A.I. ; SORKIN,L.I.

Report Date : 02 MAY 1962

Pagination or Media Count : 1

Abstract : INVESTIGATIONS WERE CONDUCTED ON THE PHYSICAL PICTURE OF THE FLOW IN THE REGION OF A STRAIGHT COMPRESSION SHOCK AND THE LOCALIZATION OF THE SEPARATION THAT OCCURS AS A RESULT OF THE INTER-ACTION BETWEEN A STRAIGHT COMPRESSION SHOCK AND THE BOUNDARY LAYER. (Author)

Descriptors :   *BOUNDARY LAYER, *SHOCK WAVES, *SUBSONIC FLOW, *SUPERSONIC FLOW, *TURBULENCE, *VISCOSITY, *WIND TUNNELS, CYLINDRICAL BODIES, FUNCTIONS(MATHEMATICS), MACH NUMBER, NOZZLES, PRESSURE, SPARK SHADOWGRAPH PHOTOGRAPHY, TRANSLATIONS

Distribution Statement : APPROVED FOR PUBLIC RELEASE