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Efficiency of a Hot Air Curtain Provided by Fan-Shaped Holes for Anti-Icing Systems of Aircraft and Their Engines

  • AIRCRAFT AND ROCKET ENGINE THEORY
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Abstract

The paper describes the experiments of study the comparative efficiency of air film heating of convex and concave surfaces using single-row bands with fan-shaped and cylindrical holes.

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ACKNOWLEDGEMENTS

The study was financially supported by the Ministry of Science and Higher Education of the Russian Federation (contract no. 075-03-2020-051-3).

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Authors and Affiliations

  1. A. Lyul’ka Design Bureau, ul. Kasatkina 13, 129301, Moscow, Russia

    E. Yu. Marchukov & A. V. Starodumov

  2. Tupolev Kazan National Research Technical University, ul. Karla Marksa 10, 420111, Kazan, Tatarstan, Russia

    A. V. Il’inkov, A. V. Shchukin & V. V. Takmovtsev

Authors
  1. E. Yu. Marchukov
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  2. A. V. Starodumov
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  3. A. V. Il’inkov
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  4. A. V. Shchukin
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  5. V. V. Takmovtsev
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Corresponding author

Correspondence to A. V. Shchukin.

Additional information

Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2021, No. 3, pp. 140 - 145.

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Marchukov, E.Y., Starodumov, A.V., Il’inkov, A.V. et al. Efficiency of a Hot Air Curtain Provided by Fan-Shaped Holes for Anti-Icing Systems of Aircraft and Their Engines. Russ. Aeronaut. 64, 511–517 (2021). https://doi.org/10.3103/S1068799821030193

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  • DOI: https://doi.org/10.3103/S1068799821030193

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