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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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