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One-Dimensional Model of the Propulsion System Air Intake for a Supersonic Civil Aircraft

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Russian Engineering Research Aims and scope

Abstract

The development of a one-dimensional model of the engine’s air intake for a supersonic civil aircraft is discussed. This model determines the air intake’s integral parameters (the flow rate, the total pressure recovery, and the drag), taking account matching with the engine in terms of the flow rate and parameters of the operating fluid under all flight conditions. The model corresponds to a fixed-geometry convergent mixed-compression air intake with a hexagonal input cross section; it contains a wedge with swept edges.

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Funding

The work was supported by the Ministry of Science and Higher Education of the Russian Federation within the framework of the 2020–2025 program for the creation and development of Sverkhzvuk Scientific Center, contract no. 075-15-2021-605, June 24, 2021.

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Authors and Affiliations

  1. Central Institute of Aviation Motors, 111116, Moscow, Russia

    A. D. Alendar, V. G. Belova, A. S. Polev & V. A. Stepanov

  2. Moscow Aviation Institute, 125080, Moscow, Russia

    A. D. Alendar & M. V. Siluyanova

Authors
  1. A. D. Alendar
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  2. V. G. Belova
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  3. A. S. Polev
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  4. V. A. Stepanov
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  5. M. V. Siluyanova
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Correspondence to A. D. Alendar.

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Translated by B. Gilbert

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Alendar, A.D., Belova, V.G., Polev, A.S. et al. One-Dimensional Model of the Propulsion System Air Intake for a Supersonic Civil Aircraft. Russ. Engin. Res. 43, 316–321 (2023). https://doi.org/10.3103/S1068798X23040032

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  • DOI: https://doi.org/10.3103/S1068798X23040032

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