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Civil-Comp Proceedings
ISSN 1759-3433 CCP: 105
PROCEEDINGS OF THE NINTH INTERNATIONAL CONFERENCE ON ENGINEERING COMPUTATIONAL TECHNOLOGY Edited by:
Paper 27
A Parallel Agglomeration Multigrid Method for Incompressible Flow Simulations G.N. Lygidakis, S.S. Sarakinos and I.K. Nikolos
School of Production Engineering and Management, Technical University of Crete, Chania, Greece G.N. Lygidakis, S.S. Sarakinos, I.K. Nikolos, "A Parallel Agglomeration Multigrid Method for Incompressible Flow Simulations", in , (Editors), "Proceedings of the Ninth International Conference on Engineering Computational Technology", Civil-Comp Press, Stirlingshire, UK, Paper 27, 2014. doi:10.4203/ccp.105.27
Keywords: incompressible flow, RANS, three-dimensional hybrid unstructured grids, multigrid, isotropic-directional agglomeration, parallelization.
Summary
Unstructured grids have gained a significant popularity during the past years, mainly
as a result of their capability to describe accurately complex geometries with the
minimum user interaction for their generation; nevertheless, the corresponding
solvers are relatively inefficient compared with the structured ones. A remedy for
this shortcoming appears to be the multigrid methodology, based on the solution of
the flow problem on successively coarser grids. In this paper the development of a
parallel agglomeration multigrid scheme is reported, enhancing an also recently
developed academic computational fluid dynamics code, named Galatea-I, which
employs the Reynolds-averaged Navier-Stokes equations along with the shear stress
transport turbulence model, to simulate incompressible fluid flows. The fusion
strategy considers either isotropic or directional adjacent control cells' merging on a
topology-preserving framework, resembling the advancing front technique. The
multigrid accelerated iterative solution of the flow and turbulence models is
succeeded by implementing the full approximation scheme using a V-cycle
strategy, incorporated though in the full multigrid scheme. The proposed algorithm
is validated against benchmark test cases, concerning inviscid and turbulent
incompressible flow over a rectangular wing with the NACA0012 airfoil, and three-dimensional
lid driven cubic cavity laminar flow, revealing its potential for
improved computational performance.
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