한국전산유체공학회:학술대회논문집

Korean Society of Computational Fluids Engineering (한국전산유체공학회)
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Flow Analysis of Three-Dimensional Wing in Ground Effect

지면 효과를 갖는 3차원 날개의 유동해석

  • 임예훈 (한국기계연구원 비활성 가스제너레이터 사업단) ;
  • 장근식 (한국과학기술원 항공우주공학과)
  • Published : 2000.05.01
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Abstract

Ground effect of three-dimensional wing is studied. LU-factored Implicit upwind TVD scheme and Baldwin-Lomax turbulence model are used for this calculation. To investigate ground effect, NACA 4415 wing at M=0.5 calculated. Two different angles of attack and three cases of flight height are calculated. As increasing angle of attack, the ground effect becomes strong. In case of NACA 4415 wing in ground effect, strength of wing tip vortex becomes stronger than that of free flight.

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