PIV Investigation of Nacelle Chine Effects on High-Lift System Performance-Reference-Cited by-同舟云学术

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PIV Investigation of Nacelle Chine Effects on High-Lift System Performance

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Kato Hiroyuki¹,Watanabe Shigeya¹,Murayama Mitsuhiro¹,Yokokawa Yuzuru¹,Ito Takeshi¹

Affiliation:

1. Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-240

Reference6 articles.

1. 1Watanabe,S.,et.al."VelocityFieldMeasurementsofaWing-FlapConfigurationviaStereoscopicPIV",AIAA2006-0043.

2. 3Ito,T.,et.al."High-LiftDeviceTestinginJAXA6.5mx5.5mLow-speed WindTunnel",AIAA2006-3643.

3. 4Ura, H., Yokokawa, Y., Ito, T. "Phased Array Measurement of High Lift Devices in Low Speed Wind Tunnel," AIAA 2006-2565,2006.

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