CFD에 의한 파력발전용 웰즈터빈의 플랩에 관한 연구

A CFD Study on Wells Turbine Flap for Wave Power Generation

  • 김정환 ((주)IIT 연구원) ;
  • 김범석 (한국해양대학교 대학원 기계공학과) ;
  • 최민석 (목포해양대학교 기관시스템공학부) ;
  • 이연원 (부경대학교 기계공학부) ;
  • 이영호 (한국해양대학교 기계.정보공학부)
  • 발행 : 2003.12.05

초록

A numerical investigation was performed to determine the effect of airfoil on the optimum flap height using NACA0015 Wells turbine. The five double flaps which have 0.5% chord height difference were selected. A Wavier-Stokes code, CFX-TASCflow, was used to calculate the flow field of the Wells turbine. The basic feature of the Wells turbine is that even though the cyclic airflow produces oscillating axial forces on the airfoil blades, the tangential force on the rotor is always in the same direction. Geometry used to define the 3-D numerical grid is based upon that of an experimental test rig. This paper tries to analyze the optimum double flap of Wells turbine with the numerical analysis.

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