Inverse transonic airfoil design using parallel simulated annealing and computational fluid dynamics

被引：13
|
作者：
Wang, X [1 ]
Damodaran, M [1 ]
Lee, SL [1 ]
机构：
[1] Nanyang Technol Univ, Singapore 639798, Singapore
来源：
AIAA JOURNAL | 2002年 / 40卷 / 04期
关键词：
Algorithms - Computational fluid dynamics - Finite volume method - Functions - Monte Carlo methods - Navier Stokes equations - Polynomials - Simulated annealing - Transonic aerodynamics;
D O I：
10.2514/2.1714
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The inverse aerodynamic design of transonic airfoil shapes using parallel simulated annealing (PSA) and computational fluid dynamics (CFD) was discussed. The objective function was evaluated using the flow analysis module, based on the finite volume method of Navier-Stokes equations. The PSA was implemented by dividing the Markov main chain into subchains on multiple processors. Results showed that the airfoil shape is parameterized using 14 basis functions, in which 7 define the upper surface and the other 7 define the lower surface of the airfoil.
引用
收藏
页码：791 / 794
页数：4
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