Aerodynamic/Aeroacoustic testing in Anechoic Closed Test Sections of Low-Speed Wind Tunnels-Reference-Cited by-同舟云学术

Aerodynamic/Aeroacoustic testing in Anechoic Closed Test Sections of Low-Speed Wind Tunnels

Published:2010-06-07 Issue: Volume: Page:
ISSN:
Container-title:16th AIAA/CEAS Aeroacoustics Conference
language:
Short-container-title:

Author:

Ito Takeshi¹,Ura Hiroki¹,Nakakita Kazuyuki¹,Yokokawa Yuzuru¹,Ng Wing²,Burdisso Ricardo²,Iwasaki Akihito¹,Fujita Toshimi¹,Ando Norihisa¹,Shimada Naoki¹,Yamamoto Kazuomi¹

Affiliation:

1. Japan Aerospace Exploration Agency (JAXA)

2. Virginia Polytechnic Institute and State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-3750

Reference18 articles.

1. 1Chow,L.C.,et.al."LandinggearsandHighLiftDevicesAirframeNoiseResearch,"AIAA-2002-2408.

2. 2Piet,J."FlightTestInvestigationofAdd-OnTreatmentstoReduceAircraftAirframeNoise,"AIAA-2005-3007

3. 3Stoker,R.W."InvestigationsofAirframeNoiseinPressureizedWindTunnels,"AIAA-2001-2107.

4. 4Stoker, R.W., et.al. "Airframe nose source Locations of a 777 Aircraft in Flight and comparisons with past model scale tests," AIAA-2003-3232.

5. 5Horne, W.C. et.al. "Measurements of 26%-Scale 777 Airframe Noise in the NASA Ames 40- by 80-ft Wind Tunnel," AIAA-2005-2810.

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