A bifurcation study of a dynamic model of a nose landing gear mechanism subjected to external disturbances
This paper presents a new modelling approach for the analysis of landing gear mechanisms. By replacing the mechanism's rotational joints with equivalent high-stiffness elastic joints, numerical continuation methods can be applied directly to dynamic models of landing gear mechanisms. The effect...
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| Format: | Default Conference proceeding |
| Published: |
2015
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| Subjects: | |
| Online Access: | https://hdl.handle.net/2134/18691 |
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