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Solution of a direct problem of heat exchange between a cooled turbine blade and a gas by the pivot method

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Abstract

Using the pivot method we solve a third-order differential equation that describes the heat exchange of a gas with a cooled turbine blade.

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Literature cited

  1. V. I. Lokai, Izv. VUZ. Aviatsionnaya Tekhnika, No. 2 (1963).

  2. V. I. Lokai, Izv. VUZ. Aviatsionnaya Tekhnika, No. 3 (1969).

  3. A. M. Topunov and Yu. N. Kulesh, Izv. VUZ. Aviatsionnaya Tekhnika, No. 3 (1965).

  4. S. K. Godunov and V. S. Ryaben'kii, Introduction to the Theory of Difference Schemes [in Russian], Fizmatgiz (1962).

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Authors
  1. A. M. Topunov
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  2. R. D. Iosifov
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  3. N. G. Rodionov
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Additional information

Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 21, No. 3, pp. 531–536, September, 1971.

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Topunov, A.M., Iosifov, R.D. & Rodionov, N.G. Solution of a direct problem of heat exchange between a cooled turbine blade and a gas by the pivot method. Journal of Engineering Physics 21, 1186–1190 (1971). https://doi.org/10.1007/BF00826124

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  • DOI: https://doi.org/10.1007/BF00826124

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