High-Lift Device Testing in JAXA 6.5M X 5.5M Low-Speed Wind Tunnel-Reference-Cited by-同舟云学术

High-Lift Device Testing in JAXA 6.5M X 5.5M Low-Speed Wind Tunnel

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Ito Takeshi¹,Yokokawa Yuzuru¹,Ura Hiroki¹,Kato Hiroyuki¹,Mitsuo Kazunori¹,Yamamoto Kazuomi¹

Affiliation:

1. Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3643

Reference15 articles.

1. 1Hansen,H."OverviewabouttheEuropeanHighLiftResearchProgrammeEUROLIFT"AIAA2004-767

2. 2Morgan, Jr. H. L, "Experimental Test Results of Energy Efficient Transport (EET) High-Lift Airfoil in Langley Low-TurbulencePressureTunnel", NASA TM-2002-211780

3. 3Chow,L.C.,et.al."LandinggearsandHighLiftDevicesAirframeNoiseResearch,"AIAA-2002-2408.

4. 4Piet,J."FlightTestInvestigationofAdd-OnTreatmentstoReduceAircraftAirframeNoise,"AIAA-2005-3007

5. 5Stoker,R.W."InvestigationsofAirframeNoiseinPressurizedWindTunnels,"AIAA-2001-2107

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