Oct 5, 2010

Study Report on Helicopter Blade-Vortex Interaction Noise

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. You can also Subscribe to FINAL YEAR PROJECT'S by Email for more such Projects and Seminar.

Author:-Koushik, Sudarshan
Source:- DRUM

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