Development of Landing and Taxiing Response Analysis System for Aircraft with Multi-Wheels and Multi-Landing Gears

Hui Wang; Le Wang

doi:10.4028/www.scientific.net/AMM.459.511

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 459Development of Landing and Taxiing Response...

Development of Landing and Taxiing Response Analysis System for Aircraft with Multi-Wheels and Multi-Landing Gears

Abstract:

Based on the modularized conception, the landing and taxiing response analysis system for aircraft with multi-wheels and multi-landing gears was developed. Firstly, the submodels, such as the oil pole model, the buffer model, the tire model and the landing gear model should be built one by one; then, the fuselage model can be assembled by the submodels; finally, the landing and taxiing responses of the aircraft can be calculated under the specified initial conditions. An aircraft model with multi-wheels and multi-landing gears was adopted as an example to verify the feasibility and effectiveness of the software.

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Periodical:

Applied Mechanics and Materials (Volume 459)

Pages:

511-516

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.459.511

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Online since:

October 2013

Authors:

Hui Wang*, Le Wang

Keywords:

Aircraft with Multi-Wheels, Dynamic Analysis, Landing, Landing Gear, Multi-Landing Gears, Software Design, Taxiing Response

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