Truncated Method for Propeller Noise Prediction up to Low Supersonic Helical Tip Mach Numbers

Author:

Marinus Benoit1,Roger Michel2,Van den Braembussche René3,Bosschaerts Walter1

Affiliation:

1. Royal Military Academy

2. Ecole Centrale de Lyon

3. von Kármán Institute for Fluid Dynamics

Publisher

American Institute of Aeronautics and Astronautics

Cited by 6 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. Numerical Investigation of Self-Propulsion Performance and Noise Level of DARPA Suboff Model;Journal of Marine Science and Engineering;2023-06-10

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

3. 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

4. Multidisciplinary Optimization of Propeller Blades: focus on the aeroelastic results;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

5. Multidisciplinary Optimization of Propeller Blades: focus on the aeroacoustic results;17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference);2011-06-05

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