Drop test simulation for a helicopter tail landing gear
Drop test simulation for a helicopter tail landing gear
- Neue Suche nach: Podruzhin, E. G.
- Neue Suche nach: Zagidulin, A. R.
- Neue Suche nach: Podruzhin, E. G.
- Neue Suche nach: Zagidulin, A. R.
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.
Dokumentinformationen
Drop test simulation for a helicopter tail landing gear
Russian Aeronautics ; 60 , 3 ; 342-348
2017-07-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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