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익형 뒷전 형상이 날개 공력 특성에 미치는 영향

STUDY ON THE EFFECTS OF AIRFOIL TRAILING EDGE SHAPE ON THE WING AERODYNAMICS

  • 김왕현 (충남대학교 항공우주공학과) ;
  • 류기명 (충남대학교 항공우주공학과) ;
  • 김병수 (충남대학교 항공우주공학과)
  • Kim, W.H. (Dept. of Aerospace Engineering, Chungnam National Univ.) ;
  • Ryu, G.M. (Dept. of Aerospace Engineering, Chungnam National Univ.) ;
  • Kim, B.S. (Dept. of Aerospace Engineering, Chungnam National Univ.)
  • 투고 : 2014.11.26
  • 심사 : 2014.12.21
  • 발행 : 2014.12.31

초록

In the paper, a study on the analysis of the effects of trailing edge thickness on the aerodynamic characteristics of an airfoil is described. In this research, modification of the formula representing NACA symmetric airfoil is studied to change the airfoil shape with different trailing edge thickness of user's choice. According to the result of aerodynamic characteristics, as the trailing edge thickness increases the maximum lift coefficient increases while the lift-to-drag ratio decreases. In this paper flow calculation results are demonstrated and the analysis on those results and findings on the effects of non-zero thickness of trailing edge are suggested.

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참고문헌

  1. 1935, Eastman, N.J., Kenneth, E.W. and Robert M.P., "The Characteristics of 78 Related Airfoil Sections from Tests in the Variable-Density Wind Tunnel," National Advisory Committee for Aeronautics, Report No.460.
  2. 1988, Charles, L.L., "Effects of Independent Variation of Mach and Reynolds Number on the Low Speed Aerodynamic Characteristics of the NACA0012 Airfoil Section," NASA Langley Research Center, Hampton, Virginia, USA.
  3. 2011, Juan, P.M. and Alvaro, P., "CFD Analysis of Blunt Trailing Edge Airfoils Obtained Several Modification Methods," Universidad de los Andes, Bogota D.C., Colombia. Rev.ing. ISSN.0121-4993. Enero-junio de, pp.14-24.
  4. 2003, Standish, K.J. and Vandam, C.P., "Analysis of Blunt Trailing Edge Airfoils," Department of Mechanical Aeronautical Engineering, University of California, Davis, Nevada, USA.