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천이 전달 모델을 사용한 익형 유동의 예측 성능 비교

A COMPARATIVE STUDY ON PREDICTION CAPABILITY OF AIRFOIL FLOWS USING A TRANSITION TRANSPORT MODEL

  • 사정환 (건국대학교 항공우주정보시스템공학과) ;
  • 전상언 (건국대학교 항공우주정보시스템공학과) ;
  • 박수형 (건국대학교 항공우주정보시스템공학과)
  • Sa, J.H. (Aerospace Information Engineering, Konkuk University) ;
  • Jeon, S.E. (Aerospace Information Engineering, Konkuk University) ;
  • Park, S.H. (Aerospace Information Engineering, Konkuk University)
  • 투고 : 2014.03.15
  • 심사 : 2014.05.28
  • 발행 : 2014.06.30

초록

Two-dimensional prediction capability of several analysis codes, such as XFOIL, MSES, and KFLOW, is compared and analyzed based on computational results of airfoil flows. To this end the transition transport equations are coupled with the Navier-Stokes equations for the prediction of the natural transition and the separation-induced transition. Experimental data of aerodynamic coefficients are used for comparison with numerical results for the transitional flows. Numerical predictions using the transition transport model show a good agreement with experimental data. Discrepancies have been found in the prediction of the pressure drag are mainly caused by the difference in the far-field circulation correction methods.

키워드

참고문헌

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