1999
DOI: 10.1006/jcph.1999.6214
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Local Rectangular Refinement with Application to Nonreacting and Reacting Fluid Flow Problems

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Cited by 48 publications
(73 citation statements)
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“…The lid, moving with a steady and spatially uniform velocity, sets up a principal vortex and subsidiary corner vortices by viscous forces and the differentially heated lateral walls of the cavity set up a buoyant vortex flow, which opposes the principal lid-driven vortex. Our parameterization and discretization are inspired by [2]; however, in this example we do not exploit local adaptive refinement. The PETSc implementation contains uniform-refinement mesh-sequencing capabilities, applied both in a nonlinear continuation sense in the outer iteration, as described in the introduction, and as an inner iteration as part of a multigrid solver.…”
Section: Incompressible Flowmentioning
confidence: 99%
See 1 more Smart Citation
“…The lid, moving with a steady and spatially uniform velocity, sets up a principal vortex and subsidiary corner vortices by viscous forces and the differentially heated lateral walls of the cavity set up a buoyant vortex flow, which opposes the principal lid-driven vortex. Our parameterization and discretization are inspired by [2]; however, in this example we do not exploit local adaptive refinement. The PETSc implementation contains uniform-refinement mesh-sequencing capabilities, applied both in a nonlinear continuation sense in the outer iteration, as described in the introduction, and as an inner iteration as part of a multigrid solver.…”
Section: Incompressible Flowmentioning
confidence: 99%
“…In the interests of space, we leave the derivation of this velocity-vorticity form of the Navier-Stokes and energy governing equations (3.1)-(3.4) to the literature (e.g., [2] and citations therein). However, to motivate our main point, we note that the two equations with velocity components under the Laplacian operators come from differentiating the continuity equation and substituting from the definition of vorticity.…”
Section: Incompressible Flowmentioning
confidence: 99%
“…In order to verify that the accuracy of the computations is settled by the accuracy tolerances, one may define for problem (13), discretized on a uniform mesh of 1024 2 : • A quasi-exact reference solution c J qe , obtained with the Strang scheme (7) with a small and constant splitting time step of ∆t = 10 −7 ;…”
Section: Characterization Of the Numerical Performance Of The Methodsmentioning
confidence: 99%
“…This approach can then be coupled with other modeling considerations, like those presented previously, and with a suitable exploitation of modern computing capabilities. For instance, implicit time integration methods are investigated for complex applications [13,14,15,16] 2 , and efforts are also being made on computationally less demanding hybrid methods which combine implicit and explicit schemes such as IMEX [17,18] or operator splitting [19,20] techniques.…”
Section: Introductionmentioning
confidence: 99%
“…When solving such problems numerically, this solution behaviour requires a much finer grid in these high activity regions than in regions where the solution is fairly smooth. This is the case, for instance, for the equations that describe laminar flames [1]: most of the activity is concentrated in the 'flame front', a narrow area where the temperature rises steeply and chemical reactions take place. Finite element methods can quite easily cope with this, but for finite difference or finite volume methods the unstructured grids, that are a consequence of this non-uniform behaviour, are much more complicated to handle.…”
Section: Introductionmentioning
confidence: 99%