Investigation and Comparison of Implicit Smoothers Applied in Agglomeration Multigrid
Author:
Affiliation:
1. Department , Institute of Aerodynamics and Flow Technology, DLR, German Aerospace Center, 38108 Brunswick, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053367
Reference49 articles.
1. Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemes
2. Preconditioned Multigrid Methods for Compressible Flow Calculations on Stretched Meshes
3. Efficient computation of compressible and incompressible flows
4. Convergence acceleration of Runge–Kutta schemes for solving the Navier–Stokes equations
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