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A THREE-DIMENSIONAL UNSTRUCTURED FINITE VOLUME METHOD FOR ANALYSIS OF DROPLET IMPINGEMENT IN ICING

비정렬 격자 기반의 결빙 액적 해석을 위한 유한체적 기법

  • Jung, K.Y. (Specialized Graduate School of Aerospace Engineering, Gyeongsang Nat'l Univ.) ;
  • Jung, S.K. (Korea Aerospace Industries Ltd.) ;
  • Myong, R.S. (Dept. of Aerospace and System Engineering & Research Center for Aircraft Parts Technology, Gyeongsang Nat'l Univ.)
  • 정기영 (경상대학교 항공우주특성화대학원) ;
  • 정성기 (한국항공우주산업(주)) ;
  • 명노신 (경상대학교 항공우주시스템공학과 및 항공기부품기술연구소)
  • Received : 2013.01.07
  • Accepted : 2013.04.21
  • Published : 2013.06.30

Abstract

Ice accretion on the solid surface is an importance factor in assessing the performance of aircraft and wind turbine blade. Changes in the external shape due to ice accretion can greatly deteriorate the aerodynamic performance. In this study, a three-dimensional upwind-type second-order positivity-preserving finite volume CFD scheme based on the unstructured mesh topology is developed to simulate two-phase flow in atmospheric icing condition. The code is then validated by comparing with NASA IRT experimental data on the sphere. The present results of the collection efficiency are found to be in close agreement with experimental data and show improvement near the stagnation region.

Keywords

References

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