• 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