다양한 난류 모텔에 따른 익형 특성 예측

PREDICTION OF AIRFOIL CHARACTERISTICS WITH VARIOUS TURBULENCE MODELING

  • 김철완 (한국항공우주연구원, 첨단공력구조팀) ;
  • 이융교 (한국항공우주연구원, 첨단공력구조팀) ;
  • 이장연 (한국항공우주연구원, 차세대항공체계실)
  • 발행 : 2007.04.06

초록

In the present paper, some difficulties encountered in predicting airfoil characteristics are described and solutions for those problems are discussed Since drag is determined by the amounts of pressure and, especially, shear stress, accurate estimation of shear stress is very crucial. However shear stress computation is dependent on the grid density and turbulence model, it should be consistent in preparing grid and turbulence model. When the transition from laminar to turbulent happen at the middle of airfoil, CFD solver should divide the region into laminar and turbulent region based on the transition location.

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