Transonic wing shape optimization using a genetic algorithm. (English) Zbl 1084.76549
Sobieczky, Helmut (ed.), IUTAM symposium Transsonicum IV. Proceedings of the IUTAM symposium, Göttingen, Germany, 2–6 September, 2002. Dordrecht: Kluwer Academic Publishers (ISBN 1-4020-1608-5/hbk). Fluid Mech. Appl. 73, 245-252 (2003).
Summary: A method for aerodynamic shape optimization based on a genetic algorithm approach is demonstrated. The algorithm is coupled with a transonic full potential flow solver and is used to optimize the flow about transonic wings including multi-objective solutions that lead to the generation of pareto fronts. The results indicate that the genetic algorithm is easy to implement, flexible in application and extremely reliable.
For the entire collection see [Zbl 1044.76012].
For the entire collection see [Zbl 1044.76012].
MSC:
| 76N25 | Flow control and optimization for compressible fluids and gas dynamics |
| 76H05 | Transonic flows |
| 76M25 | Other numerical methods (fluid mechanics) (MSC2010) |
| 92D99 | Genetics and population dynamics |
