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Engineering method of computing the radiation flux to a permeable surface under aerodynamic heating conditions

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Abstract

Formulas are proposed for the computation of the radiation heat transfer at the frontal point of an axisymmetric blunt body with a carbon-based destructible coating around which a hypersonic air stream flows.

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Authors and Affiliations

  1. A. V. Lykov Institute of Heat and Mass Transfer, Academy of Sciences of the Belorussian SSR, Minsk

    M. N. Rolin & N. L. Yadrevskaya

Authors
  1. M. N. Rolin
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  2. N. L. Yadrevskaya
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Additional information

Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 55, No. 5, pp. 763–767, November, 1988.

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Rolin, M.N., Yadrevskaya, N.L. Engineering method of computing the radiation flux to a permeable surface under aerodynamic heating conditions. Journal of Engineering Physics 55, 1241–1244 (1988). https://doi.org/10.1007/BF00872618

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  • DOI: https://doi.org/10.1007/BF00872618

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