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Inverse Design of Airfoils Based on a Novel Formulation of the Ant Colony Optimization Method 

Authors: Georgios E. Fainekos a; Kyriakos C. Giannakoglou a
Affiliation:   a National Technical University of Athens, P.O. Box 64069, Athens 15710, Greece.
DOI: 10.1080/1068276031000074288
Publication Frequency: 8 issues per year
Published in: journal Inverse Problems in Science and Engineering, Volume 11, Issue 1 2003 , pages 21 - 38
Number of References: 13
Formats available: PDF (English)
Previously published as: Inverse Problems in Engineering (1068-2767, 1029-0281) until 2004
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Abstract

In the past, Ant Colony Optimization (ACO) methods were used to solve combinatorial optimization problems such as the well-known Traveling Salesman Problem. The present article introduces an extension of the ACO method that is capable of solving optimization problems involving free variables with continuous search spaces. To this purpose, various notions, which are implicit in the ACO techniques, have been modified in order to account for design parameters that may vary continuously between lower and upper user-defined bounds. The intention was to create a tool for a particular class of engineering problems, namely the inverse design of isolated or turbomachinery blade airfoils and to demonstrate its effectiveness. Computational Fluid Dynamics codes are used for the evaluation of candidate solutions.
Keywords: Ant Colony Optimization; Inverse Design Of Aerodynamic Shapes; Optimization Algorithms
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