DocumentCode :
2929554
Title :
Icing Scaling Method on Aircraft and Verification Test
Author :
Liu Haili ; Xing Yuming ; Xu Liuqing
Author_Institution :
Sch. of Aeronaut. Sci. & Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear :
2011
fDate :
25-28 March 2011
Firstpage :
1
Lastpage :
5
Abstract :
This paper provides two methods to scale icing test conditions. The first is the Olsen method which can be used to scale the liquid-water content, and the second is the AEDC(Ruff) method which is used when the size of test model is smaller than the full size. On this basis, calculation interface of scale methods were programmed. AEDC method was evaluated by performing icing test in the YBF-02 icing tunnel. The result indicates that the similarity of the ice shape on AEDC method is acceptable.
Keywords :
aerospace engineering; aerospace safety; ice; mechanical testing; wind tunnels; AEDC method; Olsen method; YBF-02 icing tunnel; aircraft testing; icing scaling method; Aircraft; Atmospheric modeling; Equations; Ice; Mathematical model; Shape; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Power and Energy Engineering Conference (APPEEC), 2011 Asia-Pacific
Conference_Location :
Wuhan
ISSN :
2157-4839
Print_ISBN :
978-1-4244-6253-7
Type :
conf
DOI :
10.1109/APPEEC.2011.5748521
Filename :
5748521
Link To Document :
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