Aerodynamic optimization designing of airfoil based on Isight

Wei Wang; Rong Mo; Zhiyong Chang; Huibin Sun

doi:10.1109/PIC.2010.5687451

Aerodynamic optimization designing of airfoil based on Isight

Wei Wang, Rong Mo, Zhiyong Chang, Huibin Sun

School of Mechanical Engineering

Northwestern Polytechnical University Xian

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

2 Scopus citations

Abstract

In order to improving the designing efficiency and achieving automation of airfoil optimization designing, A method which combined the airfoil parametric modeling softwareinverted commas 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.

Original language	English
Title of host publication	Proceedings of the 2010 IEEE International Conference on Progress in Informatics and Computing, PIC 2010
Pages	262-266
Number of pages	5
DOIs	https://doi.org/10.1109/PIC.2010.5687451
State	Published - 2010
Event	2010 1st IEEE International Conference on Progress in Informatics and Computing, PIC 2010 - Shanghai, China Duration: 10 Dec 2010 → 12 Dec 2010

Publication series

Name	Proceedings of the 2010 IEEE International Conference on Progress in Informatics and Computing, PIC 2010
Volume	1

Conference

Conference	2010 1st IEEE International Conference on Progress in Informatics and Computing, PIC 2010
Country/Territory	China
City	Shanghai
Period	10/12/10 → 12/12/10

Keywords

Aerodynamic optimization designing of airfoil
Isight Design of Experiment(DOE)
Non-dominated Sorting Genetic Algorithm (NSGA-II)

Access to Document

10.1109/PIC.2010.5687451

Cite this

Wang, W., Mo, R., Chang, Z., & Sun, H. (2010). Aerodynamic optimization designing of airfoil based on Isight. In Proceedings of the 2010 IEEE International Conference on Progress in Informatics and Computing, PIC 2010 (pp. 262-266). Article 5687451 (Proceedings of the 2010 IEEE International Conference on Progress in Informatics and Computing, PIC 2010; Vol. 1). https://doi.org/10.1109/PIC.2010.5687451

@inproceedings{4498d4d9f9c54a0ab81e9a67a89c7086,

title = "Aerodynamic optimization designing of airfoil based on Isight",

abstract = "In order to improving the designing efficiency and achieving automation of airfoil optimization designing, A method which combined the airfoil parametric modeling softwareinverted commas 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 = "Aerodynamic optimization designing of airfoil, Isight Design of Experiment(DOE), Non-dominated Sorting Genetic Algorithm (NSGA-II)",

author = "Wei Wang and Rong Mo and Zhiyong Chang and Huibin Sun",

year = "2010",

doi = "10.1109/PIC.2010.5687451",

language = "英语",

isbn = "9781424467860",

series = "Proceedings of the 2010 IEEE International Conference on Progress in Informatics and Computing, PIC 2010",

pages = "262--266",

booktitle = "Proceedings of the 2010 IEEE International Conference on Progress in Informatics and Computing, PIC 2010",

note = "2010 1st IEEE International Conference on Progress in Informatics and Computing, PIC 2010 ; Conference date: 10-12-2010 Through 12-12-2010",

}

Wang, W, Mo, R, Chang, Z & Sun, H 2010, Aerodynamic optimization designing of airfoil based on Isight. in Proceedings of the 2010 IEEE International Conference on Progress in Informatics and Computing, PIC 2010., 5687451, Proceedings of the 2010 IEEE International Conference on Progress in Informatics and Computing, PIC 2010, vol. 1, pp. 262-266, 2010 1st IEEE International Conference on Progress in Informatics and Computing, PIC 2010, Shanghai, China, 10/12/10. https://doi.org/10.1109/PIC.2010.5687451

Aerodynamic optimization designing of airfoil based on Isight. / Wang, Wei; Mo, Rong; Chang, Zhiyong et al.
Proceedings of the 2010 IEEE International Conference on Progress in Informatics and Computing, PIC 2010. 2010. p. 262-266 5687451 (Proceedings of the 2010 IEEE International Conference on Progress in Informatics and Computing, PIC 2010; Vol. 1).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Aerodynamic optimization designing of airfoil based on Isight

AU - Wang, Wei

AU - Mo, Rong

AU - Chang, Zhiyong

AU - Sun, Huibin

PY - 2010

Y1 - 2010

N2 - In order to improving the designing efficiency and achieving automation of airfoil optimization designing, A method which combined the airfoil parametric modeling softwareinverted commas 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.

AB - In order to improving the designing efficiency and achieving automation of airfoil optimization designing, A method which combined the airfoil parametric modeling softwareinverted commas 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.

KW - Aerodynamic optimization designing of airfoil

KW - Isight Design of Experiment(DOE)

KW - Non-dominated Sorting Genetic Algorithm (NSGA-II)

UR - http://www.scopus.com/inward/record.url?scp=79951476188&partnerID=8YFLogxK

U2 - 10.1109/PIC.2010.5687451

DO - 10.1109/PIC.2010.5687451

M3 - 会议稿件

AN - SCOPUS:79951476188

SN - 9781424467860

T3 - Proceedings of the 2010 IEEE International Conference on Progress in Informatics and Computing, PIC 2010

SP - 262

EP - 266

BT - Proceedings of the 2010 IEEE International Conference on Progress in Informatics and Computing, PIC 2010

T2 - 2010 1st IEEE International Conference on Progress in Informatics and Computing, PIC 2010

Y2 - 10 December 2010 through 12 December 2010

ER -

Aerodynamic optimization designing of airfoil based on Isight

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this