2020
DOI: 10.2514/1.j059616
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Randomized Algorithms for Non-Intrusive Parametric Reduced Order Modeling

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Cited by 17 publications
(6 citation statements)
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“…where F 1 and G 1 capture the range and corange of X 1 , respectively, while H 1 is called the core sketch and describes how X 1 acts between the spaces captured by sketches F 1 and G 1 [54]. Now, near-optimal bases for the range and corange of X 1 are computed by the thin QR factorization of F 1 and G 1 as follows:…”
Section: B Sketching the Range Of Xmentioning
confidence: 99%
“…where F 1 and G 1 capture the range and corange of X 1 , respectively, while H 1 is called the core sketch and describes how X 1 acts between the spaces captured by sketches F 1 and G 1 [54]. Now, near-optimal bases for the range and corange of X 1 are computed by the thin QR factorization of F 1 and G 1 as follows:…”
Section: B Sketching the Range Of Xmentioning
confidence: 99%
“…The use of ROMs in aerospace applications has been primarily in advanced Computational Fluid Dynamics applications such as those involving unsteady aerodynamics, aero-elastic effects, hypersonic flow fields etc. [21][22][23][24][25]. These models have also been used for multi-disciplinary design, analysis, and optimization applications such as the design optimization of airfoils [26].…”
Section: Reduced Order Modelingmentioning
confidence: 99%
“…Firstly, the snapshot matrix becomes very large for problems with many time steps and parameter samples, leading to expensive singular-value decomposition (SVD). For this issue, methods such as the randomized SVD algorithm [31], fast adaptive cross-approximation [32], and local bases solutions method [33] have been used for large-scale problems. Beyond this, Wang et al [34] applied POD twice to reduce the cost of global spatial bases for unsteady flow problems in the parameter domain.…”
Section: Introductionmentioning
confidence: 99%