Affiliation:
1. University of the West of England
Publisher
American Institute of Aeronautics and Astronautics
Reference22 articles.
1. Propeller Performance at Large Angle of Attack Applicable to Compound Helicopters
2. Rotorcraft blade-vortex interaction noise prediction using the Lattice-Boltzmann method
3. ANSYS, ANSYS Fluent Theory Guide, 2021, Chap. 11: Aerodynamically Generated Noise, pp.405-420. URLhttps: //dl.cfdexperts.net/cfd_resources/Ansys_Documentation/Fluent/Ansys_Fluent_Theory_Guide.pdf.