TY - GEN
T1 - Aerodynamic optimization design of airfoil based on directly manipulated FFD technique
AU - Bai, Jun Qiang
AU - Chen, Song
PY - 2013
Y1 - 2013
N2 - The method of applying direct manipulated FFD (DFFD) technique into aerodynamic shape optimization has been proposed and researched. Due to the disadvantage of the original FFD method within which the geometrical manipulation is not direct and intuitive, the DFFD approach has been developed by solving each displacement of the FFD control points with some specified geometry points' movements, so that the deformation of the target geometry could be directly manipulated. Besides, it has been illustrated that by DFFD method a relatively small number of design variables together with high order FFD control frame could be accomplished. The study cases has shown that applying this method in aerodynamic shape optimization of airfoil for drag reduction is of good feasibility and result, and could be coupled with effective geometrical constraints like airfoil thickness.
AB - The method of applying direct manipulated FFD (DFFD) technique into aerodynamic shape optimization has been proposed and researched. Due to the disadvantage of the original FFD method within which the geometrical manipulation is not direct and intuitive, the DFFD approach has been developed by solving each displacement of the FFD control points with some specified geometry points' movements, so that the deformation of the target geometry could be directly manipulated. Besides, it has been illustrated that by DFFD method a relatively small number of design variables together with high order FFD control frame could be accomplished. The study cases has shown that applying this method in aerodynamic shape optimization of airfoil for drag reduction is of good feasibility and result, and could be coupled with effective geometrical constraints like airfoil thickness.
KW - Aerodynamic optimization design
KW - Airfoil
KW - Directly manipulated FFD
KW - Geometric constraints
KW - Geometric parameterization
UR - http://www.scopus.com/inward/record.url?scp=84884746507&partnerID=8YFLogxK
U2 - 10.4028/www.scientific.net/AMM.390.121
DO - 10.4028/www.scientific.net/AMM.390.121
M3 - 会议稿件
AN - SCOPUS:84884746507
SN - 9783037858332
T3 - Applied Mechanics and Materials
SP - 121
EP - 128
BT - Mechanical and Aerospace Engineering IV
T2 - 2013 4th International Conference on Mechanical and Aerospace Engineering, ICMAE 2013
Y2 - 20 July 2013 through 21 July 2013
ER -