Dynamic Characteristics of Aircraft Landing Gear

Jing Wei Yu; Xiao Feng Liu; Hai Long Wang; Yu Jian Wei

doi:10.4028/www.scientific.net/AMM.543-547.118

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 543-547Dynamic Characteristics of Aircraft Landing Gear

Dynamic Characteristics of Aircraft Landing Gear

Abstract:

Aircraft landing gear can absorb the energy generated and consumed in aircraft landing, taxiing process, thus weakening the vibration of the aircraft, flight safety plays a vital role. This paper established a landing gear dynamics modeling, its mechanical analysis, and through trial and simulation of the dynamic characteristics of the landing gear were studied, with some practical significance.

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Periodical:

Applied Mechanics and Materials (Volumes 543-547)

Pages:

118-121

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.543-547.118

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Online since:

March 2014

Authors:

Jing Wei Yu*, Xiao Feng Liu, Hai Long Wang, Yu Jian Wei

Keywords:

Buffer, Landing Gear, Test

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* - Corresponding Author

References

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