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Mathematical Model of a Single-Rotor Wheeled Helicopter Landing in Standard Conditions and Special Cases

  • FLIGHT DYNAMICS AND CONTROL OF FLIGHT VEHICLES
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Abstract

The main provisions of the methodology for calculating the landing of a helicopter on a tricycle wheeled landing gear, taking into account all the necessary design features of this type of landing gear and the peculiarities of the main rotor near the ground surface, are described. The comparison of computational studies with experimental data obtained during flight tests of the Mi-38 helicopter is presented.

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Authors and Affiliations

  1. National Helicopter Center Mil and Kamov, ul. Garshina 26/1, 140070, Tomilino, Moscow oblast, Russia

    M. M. Kruchinin

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

    B. L. Artamonov

Authors
  1. M. M. Kruchinin
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  2. B. L. Artamonov
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Correspondence to B. L. Artamonov.

Additional information

Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2021, No. 4, pp. 55 - 64.

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Kruchinin, M.M., Artamonov, B.L. Mathematical Model of a Single-Rotor Wheeled Helicopter Landing in Standard Conditions and Special Cases. Russ. Aeronaut. 64, 636–645 (2021). https://doi.org/10.3103/S1068799821040085

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  • DOI: https://doi.org/10.3103/S1068799821040085

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