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Investigation of Modeling Possibility for Lagging of a Helicopter Operating in Transient Flight Regimes

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  • Flight Dynamics and Control of Flight Vehicles
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Abstract

An invitational method is proposed for modeling transient loading processes of a helicopter during a flight. Formulas are presented, which allow performing imitation of lagging. An example of numerical modeling for a transient flight regime is presented.

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Authors and Affiliations

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

    A. M. Girfanov & O. A. Ledyankina

  2. Kazan State Power Engineering University, ul. Krasnosel’skaya 51, Kazan, 420066 Tatarstan, Russia

    R. Sh. Gimadiev

Authors
  1. A. M. Girfanov
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  2. O. A. Ledyankina
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  3. R. Sh. Gimadiev
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Corresponding author

Correspondence to O. A. Ledyankina.

Additional information

Russian Text © The Author(s), 2019, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2019, No. 4, pp. 176–178.

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Girfanov, A.M., Ledyankina, O.A. & Gimadiev, R.S. Investigation of Modeling Possibility for Lagging of a Helicopter Operating in Transient Flight Regimes. Russ. Aeronaut. 62, 719–721 (2019). https://doi.org/10.3103/S1068799819040263

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  • DOI: https://doi.org/10.3103/S1068799819040263

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