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Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory

  • Structural Mechanics and Strength of Flight Vehicles
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Abstract

Safety factors of the Ansat helicopter main rotor blade are determined in the root section at various flight modes with taking into account the possible damages.

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Authors and Affiliations

  1. Chistopol branch “Vostok”, Tupolev Kazan National Research Technical University, ul. Engelsa 127a, Chistopol, 422981, Tatarstan, Russia

    A. V. Gorelov

  2. PAO Kazan Helicopters, ul. Tetsevskaya 14, Kazan, 420085, Tatarstan, Russia

    E. I. Nikolaev

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

    I. N. Sidorov

Authors
  1. A. V. Gorelov
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  2. E. I. Nikolaev
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  3. I. N. Sidorov
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Corresponding author

Correspondence to A. V. Gorelov.

Additional information

Original Russian Text © A.V. Gorelov, E.I. Nikolaev, I.N. Sidorov, 2016, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2016, No. 3, pp. 13–19.

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Gorelov, A.V., Nikolaev, E.I. & Sidorov, I.N. Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory. Russ. Aeronaut. 59, 308–315 (2016). https://doi.org/10.3103/S106879981603003X

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  • DOI: https://doi.org/10.3103/S106879981603003X

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