Accession Number : AD0780377
Title : Research on Heat Transfer in Spheres and Thin Cones in the Hypersonic Flow of a Rarefied Gas,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Nikolskii,Yu V. ; Pervushin,G. E. ; Chernikova,L. G.
Report Date : 19 APR 1974
Pagination or Media Count : 14
Abstract : The research sheds light on heat transfer in spheres and thin cones at a zero angle of attack. The investigations were conducted in a vacuum wind tunnel at Mach numbers M = 4.9-9.5, and Reynold numbers Re0 = 35-1 for spheres, and Re0 = 100-4 for cones; this corresponds to the transition range between free-molecular flow and the flow of a continuous medium. The procedure used was the measurement of the total heat flow under standard conditions with compensation of heat losses in a sting, and an independent measurement of the radiant heat flux. A comparison of the data with the results of the theoretical calculation was made.
Descriptors : *Spheres, *Conical bodies, *Hypersonic flow, *Heat transfer, Angle of attack, Wind tunnel models, Translations, USSR
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE