Research Article
Multidisciplinary shape optimization in aerodynamics and electromagnetics using genetic algorithms
Article first published online: 26 MAY 1999
DOI: 10.1002/(SICI)1097-0363(19990530)30:2<149::AID-FLD829>3.0.CO;2-B
Copyright © 1999 John Wiley & Sons, Ltd.
Issue
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International Journal for Numerical Methods in Fluids
Special Issue: ECCOMAS '96
Volume 30, Issue 2, pages 149–159, 30 May 1999
Additional Information
How to Cite
Mäkinen, R. A., Periaux, J. and Toivanen, J. (1999), Multidisciplinary shape optimization in aerodynamics and electromagnetics using genetic algorithms. International Journal for Numerical Methods in Fluids, 30: 149–159. doi: 10.1002/(SICI)1097-0363(19990530)30:2<149::AID-FLD829>3.0.CO;2-B
Publication History
- Issue published online: 26 MAY 1999
- Article first published online: 26 MAY 1999
Funded by
- The Academy of Finland. Grant Number: 34063
- Abstract
- References
- Cited By
Keywords:
- shape optimization;
- genetic algorithms;
- fluid dynamics;
- electromagnetics
Abstract
A multiobjective multidisciplinary design optimization (MDO) of two-dimensional airfoil is presented. In this paper, an approximation for the Pareto set of optimal solutions is obtained by using a genetic algorithm (GA). The first objective function is the drag coefficient. As a constraint it is required that the lift coefficient is above a given value. The CFD analysis solver is based on the finite volume discretization of the inviscid Euler equations. The second objective function is equivalent to the integral of the transverse magnetic radar cross section (RCS) over a given sector. The computational electromagnetics (CEM) wave field analysis requires the solution of a two-dimensional Helmholtz equation which is obtained using a fictitious domain method. Numerical experiments illustrate the above evolutionary methodology on an IBM SP2 parallel computer. Copyright © 1999 John Wiley & Sons, Ltd.

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