DocumentCode
3397306
Title
Icing Scaling Method Numerical Validated for Airfoil Profile
Author
Chen, Yiwen ; Xing, Yuming ; Sheng, Qiang
Author_Institution
Sch. of Aeronaut. Sci. & Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear
2012
fDate
27-29 March 2012
Firstpage
1
Lastpage
5
Abstract
To the problem existing freezing test equipment unable to satisfy the demand of experimental research study on test technique of ice accretion. This paper firstly introduces two kinds of conventional icing scaling method: Olsen method and AEDC method ( Ruff ); Then using the mixed scale test model do icing test, mainly uses the simple cylindrical models do a simplified testing, thus validating the feasibility of AEDC (mixed shrinkage ratio test model ) method; Finally, in accordance with the designed airfoil mixed models for numerical simulation, thus further proved the feasibility that the hybrid scaled models instead of the original size model. The test established a scaled theory basis for numerical simulation on hybrid complex models, thereby validated the feasibility of the icing research method.
Keywords
aerospace components; air safety; aircraft testing; freezing; ice; wind tunnels; AEDC method; Olsen method; airfoil mixed models; airfoil profile; hybrid complex model; ice accretion test technique; icing scaling method; mixed shrinkage ratio test model method; Atmospheric modeling; Automotive components; Equations; Ice; Mathematical model; Numerical models; Shape;
fLanguage
English
Publisher
ieee
Conference_Titel
Power and Energy Engineering Conference (APPEEC), 2012 Asia-Pacific
Conference_Location
Shanghai
ISSN
2157-4839
Print_ISBN
978-1-4577-0545-8
Type
conf
DOI
10.1109/APPEEC.2012.6307569
Filename
6307569
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