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Temperature of a thermally insulated surface in a gas flow

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Abstract

An equation is derived for determining the temperature of a thermally insulated surface in a gas flow. The equation does not contain any empirical coefficients. The derivation is based on allowance for the work done by a jet arrested at an obstructing surface on the surrounding flow layers. The application of the equation to subsonic and supersonic flows is discussed.

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References

  1. G. N. Abramovich, Applied Gas Dynamics [in Russian], Nauka, Moscow (1976), 888 pp.

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  2. L. G. Loitsyanskii, Mechanics of Liquids and Gases [in Russian], Nauka, Moscow (1987), 840 pp.

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Authors and Affiliations

  1. Institute of Chemistry and Technology of Rare Elements and Mineral Raw Materials, Kol’skii Science Center, Russian Academy of Sciences, 184200, Apatity, Murmansk Province, Russia

    A. F. Gutsol

Authors
  1. A. F. Gutsol
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Additional information

Zh. Tekh. Fiz. 68, 134–135 (April 1998)

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Gutsol, A.F. Temperature of a thermally insulated surface in a gas flow. Tech. Phys. 43, 469–470 (1998). https://doi.org/10.1134/1.1259007

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  • DOI: https://doi.org/10.1134/1.1259007

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