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Heat transfer on the spreading line of a sweptback cylinder in an inhomogeneous hypersonic flow

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Abstract

A method is proposed for calculating heat transfer on the spreading line of blunt edges with moderate sweepback; it takes into account the influence of absorption of the inviscid vorticity of the flow by the boundary layer.

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Literature cited

  1. B. A. Zemlyanskii, “Hypersonic nonuniform flow of gas over a yawed blunt edge,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 6 (1966).

  2. V. V. Lunev, Hypersonic Aerodynamics [in Russian], Mashinostroenie, Moscow (1975).

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  3. V. V. Lunev, “The method of mean-mass variables for a boundary layer in an exterior flow with transverse inhomogeneity,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 1 (1967).

  4. B. A. Zemlyanskii, “Calculation of the heat transfer on the spreading lines of a threedimensional boundary layer in an inhomogeneous external flow,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 1 (1975).

  5. V. S. Avduevskii, B. M. Galitseiskii, G. A. Glebov et al., Fundamentals of Heat Transfer in Aeronautics and Rocket Technology [in Russian], Mashinostroenie, Moscow (1975).

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  6. E. Reshotko and J. Beckwith, “Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number,” NACA Rep. No. 1379 (1958).

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Authors and Affiliations

  1. Moscow

    B. A. Zemlyanskii & G. A. Shmanenkova

Authors
  1. B. A. Zemlyanskii
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  2. G. A. Shmanenkova
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 175–179, July–August, 1980.

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Zemlyanskii, B.A., Shmanenkova, G.A. Heat transfer on the spreading line of a sweptback cylinder in an inhomogeneous hypersonic flow. Fluid Dyn 15, 624–627 (1980). https://doi.org/10.1007/BF01089630

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  • DOI: https://doi.org/10.1007/BF01089630

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