Accession Number : AD0614629

Title :   EXPERIMENTAL INVESTIGATION OF INTERACTION OF COMPRESSION SHOCKS AND THE BOUNDARY LAYER IN THE RANGE OF MACH NUMBERS BETWEEN = 1.0 AND 1.8,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Grodzovskii,G. L.

Report Date : 15 MAR 1965

Pagination or Media Count : 24

Descriptors :   (*SHOCK WAVES, BOUNDARY LAYER), (*SUPERSONIC FLOW, SEPARATION), (*BOUNDARY LAYER, SEPARATION), AIRFOILS, TURBULENT BOUNDARY LAYER, NOZZLES, FLAT PLATE MODELS, USSR

Distribution Statement : APPROVED FOR PUBLIC RELEASE