Performance optimisation of aerodynamic shapes plays a critical role in aeronautics and the automation of design tasks is an active research field. In this paper an adaptation of Genetic Algorithms to the above problem and its parallel implementation are discussed. We have empirically compared the performance of our parallel version with the sequential one. Experimental findings on a design problem are present,ed and analysed. The results have shown that the parallel approach has allowed to find innovative solutions in a much lower convergence time.

A Parallel genetic algorithm for transonic airfoil optimisation

De Falco I;Tarantino E
1995

Abstract

Performance optimisation of aerodynamic shapes plays a critical role in aeronautics and the automation of design tasks is an active research field. In this paper an adaptation of Genetic Algorithms to the above problem and its parallel implementation are discussed. We have empirically compared the performance of our parallel version with the sequential one. Experimental findings on a design problem are present,ed and analysed. The results have shown that the parallel approach has allowed to find innovative solutions in a much lower convergence time.
1995
Inglese
IEEE International Conference on Evolutionary Computation
429
434
6
0-7803-2759-4
Sì, ma tipo non specificato
Nov. 29 - Dec. 1, 1995
Perth, Australia
4
none
De Falco, I; Del Balio, R; Della Cioppa, A; Tarantino, E
273
info:eu-repo/semantics/conferenceObject
04 Contributo in convegno::04.01 Contributo in Atti di convegno
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.14243/215085
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