Component-based model for Flap Noise Prediction-Reference-Cited by-同舟云学术

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Component-based model for Flap Noise Prediction

Published:2019-05-18 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA/CEAS Aeroacoustics Conference
language:
Short-container-title:

Author:

Jiang Yi¹,Filippone Antonio²

Affiliation:

1. China Aerodynamics Research and Development Center (CARDC)

2. University of Manchester

Publisher

American Institute of Aeronautics and Astronautics

Reference35 articles.

1. Almost 40 Years of Airframe Noise Research: What Did We Achieve?

2. A second golden age of aeroacoustics?

3. Filippone, A.Aircraftnoise prediction, Prog.Aero. Sci.68 (2014), pp. 27-63. DOI:10.1016/j.paerosci.2014.02.001.10.1016/j.paerosci.2014.02.001

4. Fink,M.R.Noisecomponentmethodforairframenoise,JournalofAircraft16(10)(1979),pp.659-665.DOI:10.2514/3.58586.10.2514/3.58586

5. Guo,Y.P.,Yamamoto,K.J.andStoker,R.W.Component-basedempiricalmodelforhigh-liftsystemnoiseprediction,Journal of Aircraft40(5) (2003), pp. 914-922. DOI:10.2514/2.6867.10.2514/2.6867

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. The Use of Porous Meshes to Reduce Landing Gear Wake - Flap Interaction Noise;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13

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