Drop test simulation for a helicopter tail landing gear

Autor:	A. R. Zagidulin, E. G. Podruzhin
Rok vydání:	2017
Předmět:	Computer Science::Robotics Computer science Drop tests Aerospace Engineering Multibody system Drop test Marine engineering Landing gear
Zdroj:	Russian Aeronautics. 60:342-348
ISSN:	1934-7901 1068-7998
DOI:	10.3103/s1068799817030047
Popis:	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.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::feb2dff0d865cb09c795da368251c6a4 https://doi.org/10.3103/s1068799817030047 Zobrazit plný text záznamu Full text from SpringerLink