한국전산유체공학회:학술대회논문집

Korean Society of Computational Fluids Engineering (한국전산유체공학회)
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Numerical Analysis and Experimental Study for Low Reynolds number region around Micro Air Vehicle

초소형 비행체 주위의 저 레이놀즈수 영역에 대한 수치 해석 및 실험적 연구

  • 김영훈 (서울대학교 항공우주공학과) ;
  • 김우례 (서울대학교 항공우주공학과) ;
  • 김종암 (서울대학교 항공우주공학과) ;
  • 노오현 (서울대학교 항공우주공학과)
  • Published : 2002.05.01
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Abstract

A three-dimensional incompressible Navier-Stokes solver is developed for the flow analysis around Micro Air Vehicle(MAV) designed by MACDL(Micro Aerodynamic Control and Design Lab), Seoul National Univ., Validations of this solver are presented for two cases, first flow over the circular cylinder with infinite length, second flow over infinite wing with wing section, E387 airfoil. Simultaneously, Wind Tunnel test is performed with Flatform Wire type sir-component balance and model designed by MACDL. The numerical results are also examined through comparison with experimental data.

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