State-of-the-art of high-speed propeller noise prediction - A multidisciplinary approach and comparison with measured data

Author:

DUNN MARK1,FARASSAT F.2

Affiliation:

1. Lockheed Engineering and Sciences Co., Hampton, VA

2. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Reference28 articles.

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Shape Sensitivities of 2D Airfoils for Broadband Noise Reduction Using the Adjoint Method and Semi-Analytical Models;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

2. Fast Prediction Model for Tonal Noise from Propellers or Rotors;22nd AIAA/CEAS Aeroacoustics Conference;2016-05-27

3. Comparative Study of Effects of Sweep and Humps on High-Speed Propeller Blades;AIAA Journal;2014-04

4. Comparative Study of the Effects of Sweep and Humps on High-Speed Propeller Blades;18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference);2012-06-04

5. Aeroacoustic and Aerodynamic Optimization of Aircraft Propeller Blades;16th AIAA/CEAS Aeroacoustics Conference;2010-06-07

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