High-speed propeller noise prediction - A multidisciplinary approach
Author:
Affiliation:
1. Lockheed Engineering & Sciences Company, Hampton Virginia 23666
2. NASA Langley Research Center, Hampton, Virginia 23665
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11128
Reference19 articles.
Cited by 9 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
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2. Adjoint-Based Aeroacoustic Design-Optimization of Flexible Rotors in Forward Flight;Journal of the American Helicopter Society;2017-10-01
3. Open Rotor Noise Prediction Using the time Domain Formulations of Farassat;International Journal of Aeroacoustics;2015-02
4. Time-Domain Approach for Acoustic Scattering of Rotorcraft Noise;Journal of the American Helicopter Society;2012-10-01
5. Truncated Method for Propeller Noise Prediction up to Low Supersonic Helical Tip Mach Numbers;15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference);2009-05-11
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