한국전산유체공학회:학술대회논문집

Korean Society of Computational Fluids Engineering (한국전산유체공학회)
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CFD ANALYSIS OF SUBSONIC AIRFOIL WIND TUNNEL TEST

아음속 익형 풍동시험 전산해석

  • 김철완 (한국항공우주연구원, 첨단공력구조팀) ;
  • 이융교 (한국항공우주연구원, 첨단공력구조팀)
  • Published : 2007.10.26
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Abstract

In the present paper, wall correction method is reviewed and applied to the numerical experimental results obtained at the wind tunnel condition. The corrected lift coefficient agrees well with the reference data generated from the grid having very far boundary. However the corrected drag coefficient presents some deviation from the reference data.

Keywords