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Aerodynamic and thermal characteristics of a body of complex shape around which a hypersonic air stream flows

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Abstract

The interaction between a sphere with a forward projecting spike and a dissociating hypersonic air flow is studied at high Reynolds numbers. The influence of the spike on the flow configuration, wave drag, and heat flux to the body surface is investigated.

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Additional information

Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 52, No. 4, pp. 547–553, April, 1987.

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Peigin, S.V., Postnikov, V.G. Aerodynamic and thermal characteristics of a body of complex shape around which a hypersonic air stream flows. Journal of Engineering Physics 52, 391–395 (1987). https://doi.org/10.1007/BF00872030

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Keywords

  • Statistical Physic
  • Heat Flux
  • Reynolds Number
  • Stream Flow
  • Body Surface