TY - GEN
T1 - Pareto-optimality-based constraint-handling technique and its application to compressor design
AU - Oyama, Akira
AU - Fujii, Kozo
AU - Shimoyama, Koji
AU - Liou, Meng Sing
N1 - Copyright:
Copyright 2020 Elsevier B.V., All rights reserved.
PY - 2005
Y1 - 2005
N2 - A new constraint-handling technique based on Pareto-optimality concept is proposed for evolutionary algorithms to efficiently deal with multiobjective multi-constraint design optimization problems. The essence of the proposed method is to apply non-dominance concept based on constraint function values to infeasible designs and to apply nondominance concept based on objective function values to feasible designs. The proposed technique does not need any constants to be tuned as the proposed technique does not use weighted-sum of constraints. First, the proposed approach is demonstrated to be remarkably more robust than traditional constraint-handling techniques through the optimal design of a welded beam and conceptual design optimization of a two-stage-to-orbit space plane. Next, high-fidelity aerodynamic design optimization of an axial compressor blade design is demonstrated.
AB - A new constraint-handling technique based on Pareto-optimality concept is proposed for evolutionary algorithms to efficiently deal with multiobjective multi-constraint design optimization problems. The essence of the proposed method is to apply non-dominance concept based on constraint function values to infeasible designs and to apply nondominance concept based on objective function values to feasible designs. The proposed technique does not need any constants to be tuned as the proposed technique does not use weighted-sum of constraints. First, the proposed approach is demonstrated to be remarkably more robust than traditional constraint-handling techniques through the optimal design of a welded beam and conceptual design optimization of a two-stage-to-orbit space plane. Next, high-fidelity aerodynamic design optimization of an axial compressor blade design is demonstrated.
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U2 - 10.2514/6.2005-4983
DO - 10.2514/6.2005-4983
M3 - Conference contribution
AN - SCOPUS:85088757041
SN - 9781624100536
T3 - 17th AIAA Computational Fluid Dynamics Conference
BT - 17th AIAA Computational Fluid Dynamics Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 17th AIAA Computational Fluid Dynamics Conference
Y2 - 6 June 2005 through 9 June 2005
ER -