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Study of heat and mass transfer for hypersonic flow past a complex body of revolution

Authors
  • Sidnyaev, N. I.1
  • 1 Bauman State Technical University, Moscow, Russia , Moscow (Russia)
Type
Published Article
Journal
Thermophysics and Aeromechanics
Publisher
Nauka/Interperiodica
Publication Date
Jan 01, 2006
Volume
13
Issue
1
Pages
17–27
Identifiers
DOI: 10.1134/S1531869906010023
Source
Springer Nature
Keywords
License
Yellow

Abstract

The experimental approach is outlined for study of heat fluxes on the surface of a blunt body of revolution (with kinked generatrix) in a hypersonic gas flow. The main attention is paid to the effect of coolant injection flow rate on resulting heat flux at different Reynolds numbers and attack angles. The significant role of distributed gas blowing on a body surface for the heat flux distribution has been demonstrated.

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