Baseline acoustic levels of the NASA active noise control fan rig

Author:

Sutliff Daniel1,Heidelberg Laurence1,Elliott David1,Nallasamy M.2

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

2. NYMA, Inc., Brook Park, OH

Publisher

American Institute of Aeronautics and Astronautics

Cited by 11 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. Noise predictions of the advanced noise control fan model using lattice Boltzmann method and Ffowcs Williams–Hawkings analogy;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2018-01

2. Effect of Weak Outlet-Guide-Vane Heterogeneity on Rotor–Stator Tonal Noise;AIAA Journal;2017-10

3. Prediction of tonal ducted fan noise;Journal of Sound and Vibration;2016-06

4. Influence and modeling of OGV heterogeneity;22nd AIAA/CEAS Aeroacoustics Conference;2016-05-27

5. Aeroacoustics research in Europe: The CEAS-ASC Report on 2005 highlights;Journal of Sound and Vibration;2007-01

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