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.
Development of Landing and Taxiing Response Analysis System for Aircraft with Multi-Wheels and Multi-Landing Gears
Applied Mechanics and Materials ; 459 ; 511-516
2013-10-31
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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