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Abstract: This paper examines the evolutionary approach for aircraft design optimization. Several niching and elitist models are first applied to Multiple-Objective Genetic Algorithms (MOGAs). Numerical results suggest that the combination of the fitness sharing and the best-N selection leads to the best performance. The resulting MOGA is then applied to multidisciplinary design optimization problems of transonic and supersonic wing planform shapes. The results confirm the feasibility of the present... (Update)
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BibTeX entry: (Update)
S. Obayashi. Multidisciplinary Design Optimization of Aircraft Wing Planform Based on Evolutionary Algorithms. In Proceedings of the 1998 IEEE International Conference on Systems, Man, and Cybernetics, La Jolla, California, IEEE, October 1998 http://citeseer.ist.psu.edu/obayashi98multidisciplinary.html More
@inproceedings{ obayashi98multidisciplinary,
author = "Shigeru Obayashi",
title = "Multidisciplinary {D}esign {O}ptimization of {A}ircraft {W}ing {P}lanform {B}ased on {E}volutionary {A}lgorithms",
booktitle = "Proceedings of the 1998 {IEEE} International Conference on Systems, Man, and Cybernetics",
publisher = "IEEE",
address = "La Jolla, California",
year = "1998",
url = "citeseer.ist.psu.edu/obayashi98multidisciplinary.html" }
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2 A numerical method for the design of camber surfaces of supe.. (context) - Carlson, Middleton
2 Inverse optimization of transonic wing shape for mid-size re.. (context) - Takahashi, Obayashi et al. - 1998
1 Navier-Stokes simulations of transonic flows over a practica.. (context) - Fujii, Obayashi - 1987
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