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ANALYSIS ON THE DYNAMIC STALL OVER AN OSCILLATING AIRFOIL USING TRANSITION TRANSPORT EQUATIONS

천이 전달 방정식을 이용한 진동하는 익형의 동적 실속의 해석

  • Jeon, S.E. (Aerospace Information Engineering, Konkuk University) ;
  • Sa, J.H. (Aerospace Information Engineering, Konkuk University) ;
  • Park, S.H. (Aerospace Information Engineering, Konkuk University) ;
  • Byun, Y.H. (Aerospace Information Engineering, Konkuk University)
  • 전상언 (건국대학교 항공우주정보시스템공학과) ;
  • 사정환 (건국대학교 항공우주정보시스템공학과) ;
  • 박수형 (건국대학교 항공우주정보시스템공학과) ;
  • 변영환 (건국대학교 항공우주정보시스템공학과)
  • Received : 2014.03.09
  • Accepted : 2014.03.19
  • Published : 2014.03.31

Abstract

Numerical investigation on the dynamic stall over an oscillating airfoil is presented. A Reynolds-Averaged Navier-Stokes (RANS) equations are coupled with transition transport equations for the natural transition. Computational results considering the turbulent transition are compared with the fully turbulent computations and the experimental data. Results with transition prediction show closer correlation with the experimental data than those with the fully turbulent assumption, especially in the reattachment region.

Keywords

References

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