DocumentCode
2069894
Title
Aerodynamic optimization designing of airfoil based on Isight
Author
Wang, Wei ; Mo, Rong ; Chang, Zhiyong ; Sun, Huibin
Author_Institution
Key Lab. of Contemporary Design & Integrated Manu.Tech., Northwestern Polytech. Univ., Xi´´an, China
Volume
1
fYear
2010
fDate
10-12 Dec. 2010
Firstpage
262
Lastpage
266
Abstract
In order to improving the designing efficiency and achieving automation of airfoil optimization designing, A method which combined the airfoil parametric modeling software, the CFD software with Isight platform was presented, it was used to optimize the airfoil to ameliorate its aerodynamic performance. During the process of optimization designing, first, we adopted the design of experiment (DOE) method to search the designing space, achieved the optimal initialization design. Then, we adopted Non-dominated Sorting Genetic Algorithm (NSGA-II) to optimize the airfoil, got the optimal airfoil aerodynamic solution. The optimized solution proved that the aerodynamic performance of the airfoil has been significantly improved, which shows the optimization designing method was reasonable and feasible.
Keywords
aerodynamics; aerospace components; computational fluid dynamics; design of experiments; genetic algorithms; CFD software; Isight; aerodynamic optimization design; airfoil parametric modeling software; design of experiment method; non dominated sorting genetic algorithm; Aerodynamics; Computational fluid dynamics; Hypercubes; Sun; Aerodynamic Optimization Designing of Airfoil; Isight Design of Experiment(DOE); Non-dominated Sorting Genetic Algorithm (NSGA-II);
fLanguage
English
Publisher
ieee
Conference_Titel
Progress in Informatics and Computing (PIC), 2010 IEEE International Conference on
Conference_Location
Shanghai
Print_ISBN
978-1-4244-6788-4
Type
conf
DOI
10.1109/PIC.2010.5687451
Filename
5687451
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