Abstract
Domain decomposition methods in finite element applied aerodynamics provides a real speed-up of the convergence and good parallel scalability, even with the minimum overlap approach used here. Furthermore, a new variant of Restricted Additive Schwarz procedure is tested and shows a very attractive scalability property.
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Chalot, F., Chevalier, G., Dinh, Q.V., Giraud, L. (1999). Some Investigations of Domain Decomposition Techniques in Parallel CFD. In: Amestoy, P., et al. Euro-Par’99 Parallel Processing. Euro-Par 1999. Lecture Notes in Computer Science, vol 1685. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-48311-X_84
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DOI: https://doi.org/10.1007/3-540-48311-X_84
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