Localisation of Flap Edge Sound Sources by Use of Spectral Analysis and Flow Investigation-Reference-Cited by-同舟云学术

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Localisation of Flap Edge Sound Sources by Use of Spectral Analysis and Flow Investigation

Published:2006-05-08 Issue: Volume: Page:
ISSN:
Container-title:12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference)
language:
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Author:

Tiedemann Christian¹,Neuwerth Günther¹

Affiliation:

1. Aachen University of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2561

Reference13 articles.

1. Large scale model measurements of airframe noise using cross‐correlation techniques

2. 4McInerny S.A., M. W. “Pressure Fluctuation in the Tip Region of a Blunt-Tipped Airfoil,” Tech. Rep. 1, 1990.

3. Measurements of unsteady pressure fluctuations on the surface of an unswept, multi-element airfoil

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. Flap-Edge Flowfield and Noise in Civil Transport Aircraft Model;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

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