2006
DOI: 10.1016/j.cma.2005.08.016
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Subgrid stabilized projection method for 2D unsteady flows at high Reynolds numbers

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Cited by 56 publications
(33 citation statements)
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“…It is well known that Galerkin techniques are not well suited for the solution of hyperbolic problems (see for instance [9]). The list of techniques aiming at addressing this issue is endless; among these methods one can cite Galerkin-Least Squares [23], Discontinuous-Galerkin [23,30], subgrid viscosity [14], method of characteristics [8], edge stabilization [5], entropy viscosity [16] and many others. We assume that the sequence of approximate densities {ρ k h } k=0,...,K ⊂ W h is obtained by one of these stabilization techniques.…”
Section: Description Of the First-order Schemementioning
confidence: 99%
“…It is well known that Galerkin techniques are not well suited for the solution of hyperbolic problems (see for instance [9]). The list of techniques aiming at addressing this issue is endless; among these methods one can cite Galerkin-Least Squares [23], Discontinuous-Galerkin [23,30], subgrid viscosity [14], method of characteristics [8], edge stabilization [5], entropy viscosity [16] and many others. We assume that the sequence of approximate densities {ρ k h } k=0,...,K ⊂ W h is obtained by one of these stabilization techniques.…”
Section: Description Of the First-order Schemementioning
confidence: 99%
“…Continuous, piecewise bilinears and biquadratics have been studied there in a two-level context. Stabilisation of both phenomena, dominating convection and violation of the discrete Babuška-Brezzi condition, are investigated in [7][8][9]23] for the incompressible Navier-Stokes equation. For the flow around a NACA 0012 airfoil, numerical results are given for Reynolds numbers up to 10 6 in [23].…”
mentioning
confidence: 99%
“…Stabilisation of both phenomena, dominating convection and violation of the discrete Babuška-Brezzi condition, are investigated in [7][8][9]23] for the incompressible Navier-Stokes equation. For the flow around a NACA 0012 airfoil, numerical results are given for Reynolds numbers up to 10 6 in [23]. Convincing are also the result of a benchmark problem of the flow around a cylinder in 2D [9] and 3D [8].…”
mentioning
confidence: 99%
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“…It is frequently advocated in the literature that linear stabilization must be supplemented with a shock capturing technique to handle properly shocks and large gradients [23,25,10,6,19]. We want to investigate the effects of combining the edge stabilization with the entropy viscosity described in the Appendix.…”
Section: Edge Stabilization Plus Entropy Viscositymentioning
confidence: 99%