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Multi-fidelity shape optimization of hydraulic turbine runner blades using a multi-objective mesh adaptive direct search algorithm
•A robust multi-fidelity optimization methodology is proposed.•It is employed in a Bi-objective optimization of Francis turbine runner blades.•It is more effective to split the computational budget among more optimization steps. A robust multi-fidelity design optimization methodology has been develo...
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Published in: | Applied mathematical modelling 2016-01, Vol.40 (2), p.1650-1668 |
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Main Authors: | , , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | •A robust multi-fidelity optimization methodology is proposed.•It is employed in a Bi-objective optimization of Francis turbine runner blades.•It is more effective to split the computational budget among more optimization steps.
A robust multi-fidelity design optimization methodology has been developed to integrate advantages of high- and low-fidelity analyses, aiming to help designers reach more efficient turbine runners within reasonable computational time and cost. An inexpensive low-fidelity inviscid flow solver handles most of the computational burden by providing data to the optimizer by evaluating objective functions and constraint values in the low-fidelity phase. An open-source derivative-free optimizer, NOMAD, explores the search space, using the multi-objective mesh adaptive direct search optimization algorithm. A versatile filtering algorithm is in charge of connecting low- and high-fidelity phases by selecting among all feasible solutions a few promising solutions which are transferred to the high-fidelity phase. In the high-fidelity phase, a viscous flow solver is used outside the optimization loop to accurately evaluate filtered candidates. High-fidelity analyses results are used to recalibrate the low-fidelity optimization problem. The developed methodology has demonstrated its ability to efficiently redesign a Francis turbine blade for new operating conditions. |
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ISSN: | 0307-904X |
DOI: | 10.1016/j.apm.2015.09.008 |