Prediction of Flap-Edge Noise Using STAR-CD-Reference-Cited by-同舟云学术

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Prediction of Flap-Edge Noise Using STAR-CD

Published:2008-05-05 Issue: Volume: Page:
ISSN:
Container-title:14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)
language:
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Author:

Waller George¹

Affiliation:

1. Bombardier Aerospace

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2863

Reference3 articles.

1. 2Storms,B.,Ross,J.,Horne,W.,Hayes,J.,Dougherty,R.,Underbrink,J.,Scharpf,D.,Moriarty,P."An AeroacousticStudy ofan Unswept WingWith aThree-Dimensional High-Lift System,"NASA TM-1998-112222, 1998

2. 3Mendonca, F., Allen, R., de Charentenay, J., Kirkham, D. "CFD Prediction of Narrowband and Broadband Cavity Acoustics At M=0.85",AIAAPaper 2003-3303

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1. Optimization of a Single-Slotted Lined Flap for Wing Trailing-Edge Noise Reduction;Journal of Aircraft;2012-07

2. Optimization of a Single Slotted Lined Flap for Airframe Noise Reduction;17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference);2011-06-05

3. Unsteady Flow and Aerodynamic Noise Analysis Around JAXA Landing Gear Model by Building-Cube Method;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

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