Title : 
Application of morphing technique to airfoil design
         
        
            Author : 
Kang, Ju Young ; Lee, B.S.
         
        
            Author_Institution : 
Dept. of Marine Technol., NTNU, Trondheim, Norway
         
        
        
        
        
        
            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;
         
        
        
        
            Conference_Titel : 
OCEANS, 2012 - Yeosu
         
        
            Conference_Location : 
Yeosu
         
        
            Print_ISBN : 
978-1-4577-2089-5
         
        
        
            DOI : 
10.1109/OCEANS-Yeosu.2012.6263576