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
Link To Document :
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