Drop test simulation for a helicopter tail landing gear |
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| Authors: | E G Podruzhin A R Zagidulin |
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| Institution: | 1.Novosibirsk State Technical University,Novosibirsk,Russia;2.S. A. Chaplygin Aeronautical Research Institute (SibNIA),Novosibirsk,Russia |
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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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