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Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System

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Abstract

This paper presents a theoretically and practically grounded architecture of design methods combination. A possibility and completeness of developing integral design solutions and intensifying the design process are provided by redistribution of emphases of numerical and natural experiments.

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Authors and Affiliations

  1. Zhukovskii National Aerospace University “Kharkiv Aviation Institute”, ul. Chkalova 17, Kharkiv, 61070, Ukraine

    A. V. Kornev & V. A. Sereda

  2. OOO HPF Rotor, ul. Rodiny 32, selo Podstepki, Stavropol’skii raion, Samara oblast, 445000, Russia

    K. V. Migalin

Authors
  1. A. V. Kornev
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  2. V. A. Sereda
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  3. K. V. Migalin
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Corresponding author

Correspondence to K. V. Migalin.

Additional information

Original Russian Text © A.V. Kornev, V.A. Sereda, K.V. Migalin, 2018, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2018, No. 1, pp. 17–25.

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Kornev, A.V., Sereda, V.A. & Migalin, K.V. Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System. Russ. Aeronaut. 61, 14–22 (2018). https://doi.org/10.3103/S1068799818010038

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  • DOI: https://doi.org/10.3103/S1068799818010038

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