Adaptive cone of influence-based blade-vortex interference signal detection
Author:
Publisher
Elsevier BV
Subject
Acoustics and Ultrasonics
Reference23 articles.
1. Helicopter flight dynamics: the theory and application of flying qualities and simulation modelling – second edition;Done;Aeronaut J,2009
2. Rotorcraft blade-vortex interaction noise prediction using the Lattice-Boltzmann method;Romani;Aerosp Sci Technol,2019
3. State-of-the-Art;Noise;J Aircraft,1978
4. Helicopter blade-vortex interaction airload and noise prediction using coupling CFD/VWM method;Zhao;Appl Sci,2017
5. Noise exposure and hearing impairment in air force pilots;Muhr;Aerosp Med Hum Perf,2019
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