Author:
Hacıogˇlu Abdurrahman,Özkol I˙brahim
Abstract
In this study, the power of vibrational genetic algorithm (VGA) for transonic airfoil design and optimisation problems, which are generally characterized by multi‐model topology in the design parameter space, has been introduced. This type of problem is characterized by search and computational time to achieve satisfying solutions. In order to obtain more robust and faster algorithm, vibration concept, our earlier study, is further developed. This developed VGA is coupled with a full potential flow‐field solver for inverse design and airfoil optimisation problem in transonic case. The performance of this implemented strategy is compared with that offered by a classical or more commonly used genetic algorithm.
Reference21 articles.
1. Baker, J.E. (1987), “Reducing bias and inefficiency in the selection algorithm”, in, Proceedings of the Second International Conference on Genetic Algorithms, Morgan Kaufmann Publishers, pp. 14–21.
2. Bock, K.W. (1990), Aerodynamic design by optimization, Paper 20, AGARD CP‐463.
3. Cao, H.V. and Bloom, G.A. (1996), Navier‐Stokes/genetic optimization of multi‐element airfoils, AIAA 96‐2487.
4. Doorly, D.J. and Peiro, L. (1997), Supervised parallel genetic algorithms in aerodynamic optimisation, AIAA 97‐1852.
5. Ermis¸, M., Ülengin, F. and Hacıogˇlu, A. (2002), Vibrational genetic algorithm (VGA) for solving continuous covering location problems, ADVIS‘2002 Second Biennial International Conference on Advances in Information Systems, 23‐25 October, İzmir, Turkey.
Cited by
21 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献