Email this article Drop test simulation for a helicopter tail landing gear
- Authors: Podruzhin E.G.1, Zagidulin A.R.2
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Affiliations:
- Novosibirsk State Technical University
- S. A. Chaplygin Aeronautical Research Institute (SibNIA)
- Issue: Vol 60, No 3 (2017)
- Pages: 342-348
- Section: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/230167
- DOI: https://doi.org/10.3103/S1068799817030047
- ID: 230167
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Abstract
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.
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About the authors
E. G. Podruzhin
Novosibirsk State Technical University
Email: t-rex27@mail.ru
Russian Federation, pr. K Marksa 20, Novosibirsk, 630073
A. R. Zagidulin
S. A. Chaplygin Aeronautical Research Institute (SibNIA)
Author for correspondence.
Email: t-rex27@mail.ru
Russian Federation, ul. Polzunova 21, Novosibirsk, 630051
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