Ray‐Acoustics Approach to Fuselage Scattering of Rotor Noise
Author:
Affiliation:
1. G.A.U.S. Dept. Mech. Eng., Univ. de Sherbrooke, Sherbrooke, Qc. Canada
Publisher
American Helicopter Society
Cited by 13 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. An accurate and efficient computational method for time-domain aeroacoustic scattering;Journal of Computational Physics;2020-07
2. Investigation of Rotor Noise Shielding Effects by the Helicopter Fuselage in Forward Flight;Journal of Aircraft;2019-07
3. Analytic Time-Domain Formulation for Acoustic Pressure Gradient Prediction in a Moving Medium;AIAA Journal;2017-08
4. Noise From Rotating Machinery;Mechanics of Flow-Induced Sound and Vibration, Volume 2;2017
5. Analytical acoustic pressure gradient prediction for moving medium problems;Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences;2015-12
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