2017
DOI: 10.1109/tevc.2016.2569018
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Efficient Use of Partially Converged Simulations in Evolutionary Optimization

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Cited by 27 publications
(12 citation statements)
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References 36 publications
(40 reference statements)
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“…For example, in aerodynamic optimization, Navier-Stokes equations or coupled boundary layer methods can be adopted, and for both methods, either 2-D or 3-D simulations can be carried out [13]. In addition, the resolution of the simulations can be adjusted by changing the resolution of the mesh size [32], or by controlling the tolerance error [4] or the maximum number of iterations [2] in CFD simulations. Therefore, the number of fidelity levels in multifidelity simulations could range from two to infinity, depending on the specific application.…”
Section: Multi-fidelity Simulationsmentioning
confidence: 99%
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“…For example, in aerodynamic optimization, Navier-Stokes equations or coupled boundary layer methods can be adopted, and for both methods, either 2-D or 3-D simulations can be carried out [13]. In addition, the resolution of the simulations can be adjusted by changing the resolution of the mesh size [32], or by controlling the tolerance error [4] or the maximum number of iterations [2] in CFD simulations. Therefore, the number of fidelity levels in multifidelity simulations could range from two to infinity, depending on the specific application.…”
Section: Multi-fidelity Simulationsmentioning
confidence: 99%
“…Resolution errors can also result from partial or incomplete simulations. For example, in CFD simulations, usually a large number of iterations are needed to accurately solve differential equations [2]. In Fig.…”
Section: A Approximation Errors In Multi-fidelity Optimizationmentioning
confidence: 99%
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“…On the other hand, the iteration for the partially converged simulation to be used as the LF simulations is set to 100, which means that the computational cost ratio between the LF and HF simulation is 0.2 for this case. This fully and partially converged simulation strategy has been employed for optimization [83,84], surrogate model construction [85], and UQ [71]. One advantage of this strategy is that some LF samples are evaluated together with the HF samples, which leads to further reduction in the computational cost.…”
Section: Transonic Airfoil In Inviscid Flowmentioning
confidence: 99%