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Formulation of the two-dimensional transient heat-conduction problem for the bladed disk of a gas turbine

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Abstract

A system of differential equations is derived for the transient heat conduction associated with a cooled gas turbine disk equipped with shrouded blades on a shank.

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Literature cited

  1. A.V. Lykov, Theory of Heat Conduction [in Russian], Vysshaya Shkola, Moscow (1967).

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  2. V. I. Lokai, Author's Abstract of Doctor's Dissertation [in Russian], Kazan Aviation Institute, Kazan (1969).

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Authors and Affiliations

  1. Aviation Technology Institute, Moscow

    E. E. Denisov & V. S. Petrovskii

Authors
  1. E. E. Denisov
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  2. V. S. Petrovskii
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Additional information

Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 21, No. 2, pp. 257–264, August, 1971.

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Denisov, E.E., Petrovskii, V.S. Formulation of the two-dimensional transient heat-conduction problem for the bladed disk of a gas turbine. Journal of Engineering Physics 21, 993–998 (1971). https://doi.org/10.1007/BF00825507

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  • DOI: https://doi.org/10.1007/BF00825507

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