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International Heat Transfer Conference 12

ISSN: 2377-424X (online)
ISSN: 2377-4371 (flashdrive)

Heat Transfer in a Heterogeneous Supersonic Flow

Eduard Borisovich Vasilevskii
Central Aerohydrodynamic Institute, Zhukovsky Moscow region, Russia

Leonid A. Dombrovsky
Joint Institute for High Temperatures, 17A Krasnokazarmennaya Str., Moscow, 111116, Russia; Tyumen State University, 6 Volodarsky Str., Tyumen, 625003, Russia

D. S. Mikhatulin
Institute of High Temperatures of the Russian Academy of Science, Moscow, Russia, 127412

Yury V. Polezhaev
Department of Heat Transfer, Institute for High Temperatures, Russian Academy of Sciences, Izhorskaya 13/19, Moscow 127412, Russia

DOI: 10.1615/IHTC12.4430
6 pages


Experimental and theoretical data on heat transfer on the surface of blunt bodies immersed in a supersonic heterogeneous flow is presented. The Mach number of the carrier free-stream gas flow is varied from 2.4 to 6, and the Reynolds number calculated on the diameter of the body immersed in a flow from 104 to 106. The mass concentration of solid particles in the flow does not exceed 3%. When the particle diameter varies from 0.15 to 160 µm, the particle velocity at collisions with the body surface varies from 0 to 1350 m/s. An analysis of the experimental data helps to develop the phenomenological model of heat transfer on the surface of a blunt body immersed in a supersonic heterogeneous flow.

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