Accession Number : AD0610329

Title :   TEMPERATURE OF A CONE IN SUPERSONIC FLOW WITH CONSIDERATION OF RADIATION,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Sokolova,I. N.

Report Date : 15 JAN 1965

Pagination or Media Count : 12

Abstract : It is shown that the solution of laminary boundary equations on a cone with consideration of the radiation effect can be reduced to the solution of equations similar to corresponding equations for a plate. It is demonstrated that the radiation of an absolutely heat conductive cone is (sq. rt. 3)/2 from the radiation of an absolutely heat conductive plate, and absolutely nonconductive cone approximately (with an accuracy of up to 2%) - (sq. rt. 3)/3 of the radiation of an absolutely non heat conductive plate. (Author)

Descriptors :   (*CONICAL BODIES, THERMODYNAMICS), (*SUPERSONIC FLOW, CONICAL BODIES), THERMAL RADIATION, THERMAL CONDUCTIVITY, MATHEMATICAL ANALYSIS, AERODYNAMIC HEATING, SURFACES, TEMPERATURE, USSR

Distribution Statement : APPROVED FOR PUBLIC RELEASE