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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

Full Bibliographic Reference for this paper
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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