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Features of Heat Transfer on a Permeable Surface in a Compressible-Gas Flow

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Abstract

A laminar compressible boundary layer on a permeable plate under blowing at small and large Prandtl numbers is investigated numerically. For Prandtl numbers Pr < 1 and the temperature of the gas blown lower than the temperature of the adiabatic impenetrable wall, the calculations carried out confirm the existence of a region of the permeable wall where the temperature is lower than the temperature of the blown gas. For Prandtl numbers Pr > 1 at a blown-gas temperature higher than that of the adiabatic impenetrable wall, the temperature of the permeable wall is higher than that of the blown gas.

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  • 02 April 2019

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REFERENCES

  1. S. S. Kutateladze and A. I. Leont’ev, Heat and Mass Transfer and Friction in Turbulent Boundary Layer (Energoatomizdat, Moscow, 1985) [in Russian].

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ACKNOWLEDGMENTS

This work was supported by the Russian Science Foundation, project no. 14-19-00499.

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Authors and Affiliations

  1. Research Institute of Mechanics, Moscow State University, 117192, Moscow, Russia

    A. I. Leont’ev, V. G. Lushchik & M. S. Makarova

  2. Bauman Moscow State Technical University, 107005, Moscow, Russia

    A. I. Leont’ev

Authors
  1. A. I. Leont’ev
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  2. V. G. Lushchik
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  3. M. S. Makarova
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Corresponding author

Correspondence to M. S. Makarova.

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Translated by V. Bukhanov

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Leont’ev, A.I., Lushchik, V.G. & Makarova, M.S. Features of Heat Transfer on a Permeable Surface in a Compressible-Gas Flow. Dokl. Phys. 63, 371–374 (2018). https://doi.org/10.1134/S1028335818090033

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  • DOI: https://doi.org/10.1134/S1028335818090033

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