2022
DOI: 10.1016/j.compfluid.2022.105385
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Unsteady physics-based reduced order modeling for large-scale compressible aerodynamic applications

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Cited by 10 publications
(1 citation statement)
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“…For example, by fixing POD bases of mass and stiffness matrices in the motion equations, the corresponding coefficients of these bases are updated by employing the first-order optimality condition on an error estimator (Dorosti, 2017). Additionally, in several aerodynamic applications, the updating of base coefficients is treated as an optimization problem solved by the Levenberg-Marquardt optimization method (Garbo and Bekemeyer, 2022;Mifsud et al, 2015) or the SNOPT toolbox (Vetrano et al, 2015). Further, to update the POD bases in reduced-order PDEs, a closed-form quadratic equation is formulated to determine the optimal scalar value in the updating formula, where the POD bases are revised by adding a scaled prior matrix (Griffiths et al, 2018).…”
Section: Literature Reviewmentioning
confidence: 99%
“…For example, by fixing POD bases of mass and stiffness matrices in the motion equations, the corresponding coefficients of these bases are updated by employing the first-order optimality condition on an error estimator (Dorosti, 2017). Additionally, in several aerodynamic applications, the updating of base coefficients is treated as an optimization problem solved by the Levenberg-Marquardt optimization method (Garbo and Bekemeyer, 2022;Mifsud et al, 2015) or the SNOPT toolbox (Vetrano et al, 2015). Further, to update the POD bases in reduced-order PDEs, a closed-form quadratic equation is formulated to determine the optimal scalar value in the updating formula, where the POD bases are revised by adding a scaled prior matrix (Griffiths et al, 2018).…”
Section: Literature Reviewmentioning
confidence: 99%