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Numerical Analysis of Aerodynamics Characteristics of Two Dimensional Airfoil Section with Elastic Flap

탄성 플랩을 갖는 2차원 날개 단면 공력 특성 전산해석

  • Won, Chang-Hee (School of Civil Engineering, Chungbuk Nat'l Univ.) ;
  • Lee, Joo-Yong (Graduate School of Civil System Engineering, Chungbuk Nat'l Univ.) ;
  • Lee, Sungsu (School of Civil Engineering, Chungbuk Nat'l Univ.)
  • 원창희 (충북대학교 토목공학과) ;
  • 이주용 (충북대학교 토목시스템 공학 대학원) ;
  • 이승수 (충북대학교 토목공학과)
  • Received : 2014.02.07
  • Accepted : 2014.03.26
  • Published : 2014.03.01

Abstract

This study presents computational analysis of aerodynamic characteristics of two-dimensional airfoil sections with elastic flap attached at the trailing edge. EDISON_CFD was utilized to simulate the incompressible turbulent flow around the foil and MIDAS_IT was employed to estimate the deflection of the flap under the pressure loading. Using iterative procedure, the terminal deflection was estimated and the resulting lift-drag ratio indicates that the favorable effect of the flap is expected within certain amount of angle of attack.

이 연구에서는 탄성 플랩이 뒷전에 장착된 2차원 날개 단면의 공력 특성을 전산 해석하였다. EDISON_CFD는 날개 주위의 비압축성 난류 유동을 시뮬레이션 하기 위해 이용되었으며, MIDAS_IT는 전산 해석 결과로 얻어진 압력 하중 하에서 탄성 플랩의 변위를 구조해석 하기 위해 사용되었다. EDISON_CFD와 MIDAS_IT의 반복 계산 절차를 이용하여, 플랩의 변위가 수렴되면 해석을 종료하여, 날개 단면에 작용하는 공력을 분석하였다. 양항비의 추정 결과 일정 받음각 이내에서 플랩의 유리한 효과가 나타날 것으로 예상된다.

Keywords

References

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