Simulation of Nose Landing Gear Shimmy with Flexible Airframe Considered
Shimmy stability of the nose landing gear of an aircraft is studied in this paper. Firstly, Shimmy model was built considering the dynamic characteristics of the airframe. Then the critical damping, critical velocity and frequency range of the shimmy are obtained by introducing relevant parameters i...
| Format: | Article |
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| Language: | zho |
| Published: |
The Northwestern Polytechnical University
2018-04-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/pdf/2018/02/jnwpu2018362p388.pdf |