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
Link To Document :
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