한국전산유체공학회:학술대회논문집

한국전산유체공학회 (Korean Society of Computational Fluids Engineering)
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에어포일의 결빙에 의한 실속 및 항력 특성 변화에 관한 CFD 해석

A CFD ANALYSIS ON EFFECTS OF ICE ACCRETIONS ON CHARACTERISTICS OF STALL AND DRAG IN AIRFOIL AERODYNAMICS

  • 정성기 (경상대학교 기계항공공학부) ;
  • 신성민 (경상대학교 기계항공공학부) ;
  • 명노신 (경상대학교 기계항공공학부 및 항공기부품기술연구소) ;
  • 조태환 (경상대학교 기계항공공학부 및 항공기부품기술연구소)
  • 발행 : 2009.04.24
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초록

The aerodynamic performance of aircraft in icing condition can deteriorate considerably by contamination of aerodynamic and propulsive systems due to icing accretions on aircraft surfaces. A computational analysis based on the Eulerian description was performed on an airfoil to investigate effects of ice accretions on airfoil aerodynamics. A water droplet with liquid water concentration ($0.00075kg/m^3$) and mean volume diameter ($20{\mu}m$) was considered and applied to various angles of attack to investigate the stall angle decrease and the drag increment.

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