2004
DOI: 10.1016/j.cma.2003.11.010
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Finite point solver for the simulation of 2-D laminar incompressible unsteady flows

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Cited by 28 publications
(38 citation statements)
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“…To begin with, the ROM developed above is applied using the 210 snapshots indicated in section 2 and retaining the 15 most energetic POD modes, calculated using the projection window (19); the residual is calculated using only 50 equispaced points in the projection window (27). Relative errors (in %) on the three figures of merit (namely, the reattachment length, the pressure drop, and the heat flux) at the test points are given in Table 2 as calculated using both HOSVD + interpolation (as described above) and the ROM; see Table 1 for the definition of the test points and the CFD-calculated valúes of the figures of merit.…”
Section: Resultsmentioning
confidence: 99%
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“…To begin with, the ROM developed above is applied using the 210 snapshots indicated in section 2 and retaining the 15 most energetic POD modes, calculated using the projection window (19); the residual is calculated using only 50 equispaced points in the projection window (27). Relative errors (in %) on the three figures of merit (namely, the reattachment length, the pressure drop, and the heat flux) at the test points are given in Table 2 as calculated using both HOSVD + interpolation (as described above) and the ROM; see Table 1 for the definition of the test points and the CFD-calculated valúes of the figures of merit.…”
Section: Resultsmentioning
confidence: 99%
“…Table 2 Relative errors resulting from both HOSVD + interpolation and ROM calculations on the reattachment length, the pressure drop, and the heat flux, using 210 snapshots and 15 modes. POD modes are calculated in the projection window (19) and the residual is calculated from 50 equispaced points in the projection window (27). The mesh used in the CFD calculations is separated into 5 different zones, as plotted in Fig.…”
Section: Methods Descriptionmentioning
confidence: 99%
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