2000•Mechanical Science and TechnologyRequires access
Analysis of the Asymmetric Landing and Taxiing Loads of Aircraft
HU Meng-quan
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Abstract
A new method to analyze the asymmetric landing and taxiing loads of aircraft is presented by way of establishing the truly simulated model of the asymmetric landing and taxiing phases of aircraft. The dynamic loads of the whole aircraft in the asymmetric landing are simulated by means of an initial roll angle of aircraft. According to the 1-cos runway specified in GJB of China, the taxiing loads of aircraft are computed. The simulated results show that this method can reasonably simulate the true loads of aircraft in its asymmetric landing and taxiing. In addition, the results can provide a new case of load for the aircraft strength design.