A Method to Predict Acoustic Scattering of Rotorcraft Noise-Reference-Cited by-同舟云学术

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A Method to Predict Acoustic Scattering of Rotorcraft Noise

Published:2009 Issue:4 Volume:54 Page:042007
ISSN:0002-8711
Container-title:Journal of the American Helicopter Society
language:en
Short-container-title:J. Am. Helicopter Society

Author:

Lee Seongkyu,Erwin James P.,Brentner Kenneth S.

Publisher

American Helicopter Society

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering,General Materials Science

Cited by 12 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. High-fidelity computational study of aerodynamic noise of side-by-side rotor in full configuration;Journal of Sound and Vibration;2024-12

2. Challenges and opportunities for low noise electric aircraft;International Journal of Aeroacoustics;2022-06-28

3. Analytic Time-Domain Formulation for Acoustic Pressure Gradient Prediction in a Moving Medium;AIAA Journal;2017-08

4. Review: The Use of Equivalent Source Method in Computational Acoustics;Journal of Computational Acoustics;2017-03

5. Comment on “Acoustic Velocity Formulation for Sources in Arbitrary Motion”;AIAA Journal;2016-05

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