Accession Number : AD0609788

Title :   CONNECTION OF AERODYNAMIC HEAT WITH SKIN FRICTION,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Kozlov,L. V.

Report Date : 01 DEC 1964

Pagination or Media Count : 10

Abstract : The article attempts to determine a more accurate dependence between heat transfer and friction in super sonic flow of gas, flowing over a flat plate, by analyzing experiments with respect to direct and simultaneous measurement of the local values of heat flow and friction.

Descriptors :   (*AERODYNAMIC HEATING, FRICTION), (*FRICTION, HEAT TRANSFER), (*HEAT TRANSFER, SUPERSONIC FLOW), BOUNDARY LAYER, ATMOSPHERE ENTRY, HEAT TRANSFER COEFFICIENTS, EXPERIMENTAL DATA, MATHEMATICAL ANALYSIS, FLAT PLATE MODELS, MEASUREMENT, WIND TUNNELS, TURBULENCE, USSR

Distribution Statement : APPROVED FOR PUBLIC RELEASE