Drop test simulation for a helicopter tail landing gear
- 作者: Podruzhin E.G.1, Zagidulin A.R.2
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隶属关系:
- Novosibirsk State Technical University
- S. A. Chaplygin Aeronautical Research Institute (SibNIA)
- 期: 卷 60, 编号 3 (2017)
- 页面: 342-348
- 栏目: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230167
- DOI: https://doi.org/10.3103/S1068799817030047
- ID: 230167
如何引用文章
详细
The paper describes a mathematical model of drop tests on the landing gear of the Ka-62 helicopter. The model is formulated using the multibody system simulation procedure based on the Lagrange equations of the first kind.
作者简介
E. Podruzhin
Novosibirsk State Technical University
Email: t-rex27@mail.ru
俄罗斯联邦, pr. K Marksa 20, Novosibirsk, 630073
A. Zagidulin
S. A. Chaplygin Aeronautical Research Institute (SibNIA)
编辑信件的主要联系方式.
Email: t-rex27@mail.ru
俄罗斯联邦, ul. Polzunova 21, Novosibirsk, 630051
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