Volume 29 Issue 6
Jun.  2014
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LU Tian, SANG Wei-min, LIU Xiao-yu, XI Chao. Numerical simulation of icing accretion and influence on three-dimensional wing configuration[J]. Journal of Aerospace Power, 2014, (6): 1339-1345. doi: 10.13224/j.cnki.jasp.2014.06.011
Citation: LU Tian, SANG Wei-min, LIU Xiao-yu, XI Chao. Numerical simulation of icing accretion and influence on three-dimensional wing configuration[J]. Journal of Aerospace Power, 2014, (6): 1339-1345. doi: 10.13224/j.cnki.jasp.2014.06.011

Numerical simulation of icing accretion and influence on three-dimensional wing configuration

doi: 10.13224/j.cnki.jasp.2014.06.011
  • Received Date: 2013-04-08
  • Publish Date: 2014-06-28
  • The structured grid was used to numerically simulate the icing accretion of M6 wing and wing-body-tail configuration to get the icing process and influence under icing weather conditions. Euler two-plase flow methods was used to solve droplets impingement characteristics for the simulation of icing process. Thermodynamic model of icing growth was based on the Messinger model. Then, it was researched that the droplet impingment, shape of the iced wing and the influence on aerodynamic characteristics. The result showed the mass of icing increased with the spanwise chord reduction, especially for high-aspect-ratio wing. Moreover, the front of fuselage was also vulnerable to serious icing.

     

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