This is Study on Helicopter Blade-Vortex Interaction Noise which is a A unique and novel experimental approach.This is good report for Aerospace Engineering which is achieved by having a non-lifting single-bladed rotor with a rigid hub interact with a carefully con- trolled gust disturbance that replicates the essential characteristics of the vortex velocity. You can use this report for your reference and study.
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Author:-Koushik, Sudarshan
Source:- DRUM
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