Application of LED Light Source in the Flow Imaging

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Abstract:

Aircraft in flight, such as supercooled water droplets encountered icing conditions suitable for the external environment, the relevant parts of the body will freeze, making the aircraft's aerodynamic performance deterioration, severe endanger flight safety, in addition, the aircraft parked in the open winter months , there will be icing, you need to clean up before takeoff. We should grasp the mechanism of aircraft icing, environmental factors and easy to freeze parts of the body. This paper presents a simulation using the wind tunnel icing device icing wind tunnel simulations can reproduce the real situation of aircraft icing, for guiding practice and got good results.

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219-222

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August 2013

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Ā© 2013 Trans Tech Publications Ltd. All Rights Reserved

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[1] Wang Yufang. Thermal fiber self-regulating anti-icing system [J]. Beijing: International Aviation, 1992, 19 (2): 22 ~ 25.

Google Scholar

[2] Hickman G A, Gerardi J J, FengY. Application of smart structures to aircraft health monitoring[J]. Journal of Intelligent Material,Systems and Structures,1991,13(3) 411~430.

DOI: 10.1177/1045389x9100200308

Google Scholar

[3] Wind tunnel test optical measurement method. [M]. Beijing:Beijing Institute of Aeronautics Press. 1985. 10.

Google Scholar

[4] Yuan Xiguang. Sensors Manual [M]. Beijing: National Defense Industry Press, (1992).

Google Scholar

[5] Wang Zongyan American ice tunnel overview [J]. Beijing: Aviation Science and Technology, 1997 (3) 45-47.

Google Scholar

[6] Yunqilinzhu Wind tunnel experiment data error correction [M]. Beijing: National Defense Industry Press, 1996. 1.

Google Scholar