• DocumentCode
    2916337
  • Title

    Application of morphing technique to airfoil design

  • Author

    Kang, Ju Young ; Lee, B.S.

  • Author_Institution
    Dept. of Marine Technol., NTNU, Trondheim, Norway
  • fYear
    2012
  • fDate
    21-24 May 2012
  • Firstpage
    1
  • Lastpage
    8
  • Abstract
    Airfoil is a cross section of a wing or blade and can be represented by polygonal lines. Although drawing an airfoil shape is an easy matter, selecting a right shape fit for the purpose is not. The shape of the airfoil profile is a key factor for good performance of the turbines, making it essential to optimise the airfoil for a maximum lift with a minimum drag. This paper discusses the use of morphing technique for a rapid airfoil generation, and it illustrates the potential of the technique as a powerful tool for the process of foil optimisation.
  • Keywords
    aerodynamics; aerospace components; curve fitting; design engineering; drag; optimisation; turbines; airfoil design; airfoil generation; airfoil profile; airfoil shape; blade; foil optimisation; maximum lift; minimum drag; morphing technique; polygonal lines; turbines; wing; Atmospheric modeling; Automotive components; Blades; Optimization; Shape; Wind turbines; airfoil generation; morphing; muti-parent morphing; optimisation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    OCEANS, 2012 - Yeosu
  • Conference_Location
    Yeosu
  • Print_ISBN
    978-1-4577-2089-5
  • Type

    conf

  • DOI
    10.1109/OCEANS-Yeosu.2012.6263576
  • Filename
    6263576