Email this article Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory
- Authors: Gorelov A.V.1, Nikolaev E.I.2, Sidorov I.N.3
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Affiliations:
- Chistopol branch “Vostok”
- PAO Kazan Helicopters
- Tupolev Kazan National Research Technical University
- Issue: Vol 59, No 3 (2016)
- Pages: 308-315
- Section: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/229739
- DOI: https://doi.org/10.3103/S106879981603003X
- ID: 229739
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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.
About the authors
A. V. Gorelov
Chistopol branch “Vostok”
Author for correspondence.
Email: a.gorelov-kai@yandex.ru
Russian Federation, ul. Engelsa 127a, Chistopol, Tatarstan, 422981
E. I. Nikolaev
PAO Kazan Helicopters
Email: a.gorelov-kai@yandex.ru
Russian Federation, ul. Tetsevskaya 14, Kazan, Tatarstan, 420085
I. N. Sidorov
Tupolev Kazan National Research Technical University
Email: a.gorelov-kai@yandex.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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