한국전산유체공학회:학술대회논문집

Korean Society of Computational Fluids Engineering (한국전산유체공학회)
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Aerodynamic Analysis of Smart UAV with CFD

CFD를 이용한 스마트 문인기의 공력특성 분석

  • 김철완 (한국항공우주연구원 공력성능그룹) ;
  • 정진덕 (한국항공우주연구원 공력성능그룹) ;
  • 이장연 (한국항공우주연구원 공력성능그룹)
  • Published : 2004.10.01
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Abstract

CFD simulation for Smart-UAV(TR-E2Sl) is performed to analyze its aerodynamic characteristics. Base geometry and several cases, decided by control surfaces being deflected, are simulated. To obtain the better lift characteristics, the elevator should be deflected between 10o and 20o with the incidence angle of the wing 1o.

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