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Mathematical Modeling of Interferential Flow around the Finned Body in the Transport Compartment and When Exiting Thereof at Subsonic Aircraft Movement

  • AERO- AND GAS-DYNAMICS OF FLIGHT VEHICLES AND THEIR ENGINES
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Abstract

The paper considers the mathematical modeling of the air flow in an empty transport compartment at a subsonic speed of the aircraft at various angles of flaps opening, as well as the flow in a cluttered compartment in the presence of a finned body of revolution placed in it. The modeling of interference flow processes around a finned body of revolution at the exit from the transport compartment was carried out.

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Authors and Affiliations

  1. AO GNPP “Region”, Kashirskoe shosse 13a, 115230, Moscow, Russia

    P. V. Tokareva

  2. Moscow Aviation Institute (National Research University), Volokolamskoe shosse 4, 125993, Moscow, Russia

    V. T. Grumondz

  3. Bauman Moscow State Technical University, ul. 2ya Baumanskaya 5, 105005, Moscow, Russia

    V. T. Kalugin

Authors
  1. P. V. Tokareva
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  2. V. T. Grumondz
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  3. V. T. Kalugin
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Corresponding author

Correspondence to V. T. Grumondz.

Additional information

Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2021, No. 4, pp. 81 - 89.

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Tokareva, P.V., Grumondz, V.T. & Kalugin, V.T. Mathematical Modeling of Interferential Flow around the Finned Body in the Transport Compartment and When Exiting Thereof at Subsonic Aircraft Movement. Russ. Aeronaut. 64, 678–687 (2021). https://doi.org/10.3103/S1068799821040127

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  • DOI: https://doi.org/10.3103/S1068799821040127

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