Investigation of Rotor Noise Shielding Effects by the Helicopter Fuselage in Forward Flight
Author:
Affiliation:
1. DLR Institute of Aerodynamics and Flow Technology, D-38108 Braunschweig, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C035009
Reference11 articles.
1. Ray‐Acoustics Approach to Fuselage Scattering of Rotor Noise
2. Simulation of Helicopter Community Noise in Complex Urban Geometry
3. Validation of a Model for Open Rotor Noise Predictions and Calculation of Shielding Effects using a Fast BEM
4. Acoustic Wind Tunnel Tests on Helicopter Tail Rotor Noise (HeliNOVI)
5. Acoustic generation by vibrating bodies in homentropic potential flow at low Mach number
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