2021
DOI: 10.2514/1.j060225
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Bayesian Optimization of a Low-Boom Supersonic Wing Planform

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Cited by 13 publications
(2 citation statements)
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“…Jim et al [143] concentrated on optimizing the aerodynamics and aeroacoustics of a hypothetical low-drag, low-boom supersonic planform using Kriging-based Bayesian multi-objective optimization and the gradient-free GA algorithm (Figure 2). The authors investigated the use of Euler Computational Fluid Dynamics (CFD) with an enhanced version of the Burgers PDE solver [144,145] and an experimental parasitic drag addition to speed up the design space exploration and multi-objective optimization processes.…”
Section: Optimization Algorithmsmentioning
confidence: 99%
“…Jim et al [143] concentrated on optimizing the aerodynamics and aeroacoustics of a hypothetical low-drag, low-boom supersonic planform using Kriging-based Bayesian multi-objective optimization and the gradient-free GA algorithm (Figure 2). The authors investigated the use of Euler Computational Fluid Dynamics (CFD) with an enhanced version of the Burgers PDE solver [144,145] and an experimental parasitic drag addition to speed up the design space exploration and multi-objective optimization processes.…”
Section: Optimization Algorithmsmentioning
confidence: 99%
“…Most aerodynamic design optimization methods using surrogate models rely on an iterative model refinement [440]. Such surrogate-based optimization strategies have shown to be effective in various aerodynamic shape optimization applications including single-point design [441,442], multipoint design [328,443], massively multipoint design [100], multi-objective design [93,444,445], inverse design [168,446], and robust design [313,[447][448][449]. Optimization using these methods is generally composed of two phases.…”
Section: Surrogate-based Optimizationmentioning
confidence: 99%