Abstract
This paper presents a two-level strategy for the parallelization of a genetic algorithm coupled to a compressible flow solver designed on unstructured meshes. The resulting algorithm is used for the optimum shape design of aerodynamic configurations. Preliminary results are presented for the optimization of two-dimensional airfoils.
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© 1997 Springer-Verlag Berlin Heidelberg
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Marco, N., Lanteri, S., Désidéri, JA., Mantel, B., Périaux, J. (1997). Parallel genetic algorithms applied to optimum shape design in aeronautics. In: Lengauer, C., Griebl, M., Gorlatch, S. (eds) Euro-Par'97 Parallel Processing. Euro-Par 1997. Lecture Notes in Computer Science, vol 1300. Springer, Berlin, Heidelberg. https://doi.org/10.1007/BFb0002826
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DOI: https://doi.org/10.1007/BFb0002826
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