Experimental Analysis of Brake Induced Vibration in the Aircraft Rolling: Technical Note
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Abstract
This paper deals with the study of vibration analysis of the rolling aircraft tyre in various frequency conditions on free and braking conditions. This paper develops mathematical model for tyre and generates dynamic equations for numerical simulations in Matlab Simulink. The experimental test facility has been developed to measure the vibration parameters while rolling the tyre with load or no load conditions. Finally, the analysis has been carried out and the levels of vibration were measured experimentally.
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