Study of the Impact of Turbulent Anisotropy on the Airfoil Turbulent Boundary Layer Trailing Edge Noise-Reference-Cited by-同舟云学术

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Study of the Impact of Turbulent Anisotropy on the Airfoil Turbulent Boundary Layer Trailing Edge Noise

Published:2016-05-27 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA/CEAS Aeroacoustics Conference
language:
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Author:

Bai Baohong¹,Li Xiaodong¹

Affiliation:

1. Beihang University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-2813

Reference32 articles.

1. BrooksT.F.,PopeD.S.andMarcoliniM.A."Airfoilself-noiseandprediction",NASA-RP-1218,1989.

2. RobertG.R.,MillerG.,GuoY.P.AndYamamotoK."AirframeNoiseStudies-ReviewandFutureDirection",NASA-CR213767, 2005.

3. TylerJ.M.andSofrinT.G."AxialFlowCompressorNoiseStudies",Trans.SAE,1962.70:309-332.

4. Turbine Noise: Its Significance in the Civil Aircraft Noise Problem

5. WagnerS.,BareibR.andGuidatiG."WindTurbineNoise",Berlin:Springer,1996.

Cited by 1 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. Turbulent boundary layer trailing-edge noise: Theory, computation, experiment, and application;Progress in Aerospace Sciences;2021-10

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