238 research outputs found
Semiannual report, 1 October 1990 - 31 March 1991
Research conducted at the Institute for Computer Applications in Science and Engineering in applied mathematics, numerical analysis, and computer science is summarized
Schnelle Löser für partielle Differentialgleichungen
[no abstract available
Implicit time integration for high-order compressible flow solvers
The application of high-order spectral/hp element discontinuous Galerkin (DG)
methods to unsteady compressible flow simulations has gained increasing popularity.
However, the time step is seriously restricted when high-order methods are applied
to an explicit solver. To eliminate this restriction, an implicit high-order compressible flow solver is developed using DG methods for spatial discretization, diagonally
implicit Runge-Kutta methods for temporal discretization, and the Jacobian-free
Newton-Krylov method as its nonlinear solver. To accelerate convergence, a block
relaxed Jacobi preconditioner is partially matrix-free implementation with a hybrid
calculation of analytical and numerical Jacobian.The problem of too many user-defined parameters within the implicit solver is
then studied. A systematic framework of adaptive strategies is designed to relax the
difficulty of parameter choices. The adaptive time-stepping strategy is based on the
observation that in a fixed mesh simulation, when the total error is dominated by the
spatial error, further decreasing of temporal error through decreasing the time step
cannot help increase accuracy but only slow down the solver. Based on a similar
error analysis, an adaptive Newton tolerance is proposed based on the idea that
the iterative error should be smaller than the temporal error to guarantee temporal
accuracy. An adaptive strategy to update the preconditioner based on the Krylov
solver’s convergence state is also discussed. Finally, an adaptive implicit solver is
developed that eliminates the need for repeated tests of tunning parameters, whose
accuracy and efficiency are verified in various steady/unsteady simulations. An improved shock-capturing strategy is also proposed when the implicit solver
is applied to high-speed simulations. Through comparisons among the forms of
three popular artificial viscosities, we identify the importance of the density term
and add density-related terms on the original bulk-stress based artificial viscosity.
To stabilize the simulations involving strong shear layers, we design an extra shearstress based artificial viscosity. The new shock-capturing strategy helps dissipate
oscillations at shocks but has negligible dissipation in smooth regions.Open Acces
The Sixth Copper Mountain Conference on Multigrid Methods, part 1
The Sixth Copper Mountain Conference on Multigrid Methods was held on 4-9 Apr. 1993, at Copper Mountain, CO. This book is a collection of many of the papers presented at the conference and as such represents the conference proceedings. NASA LaRC graciously provided printing of this document so that all of the papers could be presented in a single forum. Each paper was reviewed by a member of the conference organizing committee under the coordination of the editors. The multigrid discipline continues to expand and mature, as is evident from these proceedings. The vibrancy in this field is amply expressed in these important papers, and the collection clearly shows its rapid trend to further diversity and depth
ICASE
This report summarizes research conducted at the Institute for Computer Applications in Science and Engineering in the areas of (1) applied and numerical mathematics, including numerical analysis and algorithm development; (2) theoretical and computational research in fluid mechanics in selected areas of interest, including acoustics and combustion; (3) experimental research in transition and turbulence and aerodynamics involving Langley facilities and scientists; and (4) computer science
Artificial Compressibility Approaches in Flux Reconstruction for Incompressible Viscous Flow Simulations
Copyright © 2021 The Author(s). Several competing artificial compressibility methods for the incompressible flow equations are examined using the high-order flux reconstruction method. The established artificial compressibility method (ACM) of \citet{Chorin1967} is compared to the alternative entropically damped (EDAC) method of \citet{Clausen2013}, as well as an ACM formulation with hyperbolised diffusion. While the former requires the solution to be converged to a divergence free state at each physical time step through pseudo iterations, the latter can be applied explicitly. We examine the sensitivity of both methods to the parameterisation for a series of test cases over a range of Reynolds numbers. As the compressibility is reduced, EDAC is found to give linear improvements in divergence whereas ACM yields diminishing returns. For the Taylor--Green vortex, EDAC is found to perform well; however on the more challenging circular cylinder at , EDAC gives rise to early transition of the free shear-layer and over-production of the turbulence kinetic energy. This is attributed to the spatial pressure fluctuations of the method. Similar behaviour is observed for an aerofoil at with an attached transitional boundary layer. It is concluded that hyperbolic diffusion of ACM can be beneficial but at the cost of case setup time, and EDAC can be an efficient method for incompressible flow. However, care must be taken as pressure fluctuations can have a significant impact on physics and the remedy causes the governing equation to become overly stiff.https://arxiv.org/abs/2111.07915v
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