电邮这篇文章 Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory
- 作者: Gorelov A.1, Nikolaev E.2, Sidorov I.3
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隶属关系:
- Chistopol branch “Vostok”
- PAO Kazan Helicopters
- Tupolev Kazan National Research Technical University
- 期: 卷 59, 编号 3 (2016)
- 页面: 308-315
- 栏目: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/229739
- DOI: https://doi.org/10.3103/S106879981603003X
- ID: 229739
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详细
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.
作者简介
A. Gorelov
Chistopol branch “Vostok”
编辑信件的主要联系方式.
Email: a.gorelov-kai@yandex.ru
俄罗斯联邦, ul. Engelsa 127a, Chistopol, Tatarstan, 422981
E. Nikolaev
PAO Kazan Helicopters
Email: a.gorelov-kai@yandex.ru
俄罗斯联邦, ul. Tetsevskaya 14, Kazan, Tatarstan, 420085
I. Sidorov
Tupolev Kazan National Research Technical University
Email: a.gorelov-kai@yandex.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
