Please use this identifier to cite or link to this item: http://dspace2020.uniten.edu.my:8080/handle/123456789/8123
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dc.contributor.authorNg, K.C.-
dc.contributor.authorYusoff, M.Z.-
dc.contributor.authorNg, E.Y.K.-
dc.date.accessioned2018-02-15T02:25:00Z-
dc.date.available2018-02-15T02:25:00Z-
dc.date.issued2006-
dc.identifier.urihttp://dspace.uniten.edu.my/jspui/handle/123456789/8123-
dc.description.abstractHigh-speed compressible flows in a nozzle and over an airfoil have been computed by solving the Euler equations using the GAMMA differencing scheme for spatial discretisation on unstructured grid. This high-resolution technique originally developed in a segregated algorithm has now been modified for the present coupled solver by introducing a non-linear blending factor to enhance its convergence property while preserving the Total Variation Diminishing (TVD) criterion. The efficiencies of the GAMMA scheme and its variant have been augmented with a novel agglomeration multigrid scheme to accelerate the convergence to steady state using the multi-stage Runge-Kutta time-marching technique. Copyright © 2006 Inderscience Enterprises Ltd.-
dc.titleMultigrid solution of Euler equations using high-resolution NVD differencing scheme for unstructured meshes-
item.fulltextNo Fulltext-
item.grantfulltextnone-
Appears in Collections:COE Scholarly Publication
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