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Thermophysics and Aeromechanics

, Volume 13, Issue 1, pp 17–27 | Cite as

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

  • N. I. Sidnyaev
Article

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.

Keywords

Mass Transfer Heat Flux Reynolds Number Body Surface Injection Flow 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© N.I. Sidnyaev 2006

Authors and Affiliations

  • N. I. Sidnyaev
    • 1
  1. 1.Bauman State Technical UniversityMoscowRussia

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