Modeling of Broadband Liners Applied to the Advanced Noise Control Fan

Author:

Nark Douglas M.1,Jones Michael G.1,Sutliff Daniel L.2

Affiliation:

1. NASA Langley Research Center

2. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Reference16 articles.

Cited by 5 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. Multi-degree-of-freedom liner development: Concept to flight test;International Journal of Aeroacoustics;2021-06-28

2. An acoustic liner design methodology based on a statistical source model;International Journal of Aeroacoustics;2021-06-24

3. Design of an Advanced Inlet Liner for the Quiet Technology Demonstrator 3;25th AIAA/CEAS Aeroacoustics Conference;2019-05-18

4. Design and Acoustic Efficacy of a Broadband Liner for the Inlet of the DGEN Aero-propulsion Research Turbofan;25th AIAA/CEAS Aeroacoustics Conference;2019-05-18

5. Further Development and Assessment of a Broadband Liner Optimization Process;22nd AIAA/CEAS Aeroacoustics Conference;2016-05-27

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