Publisher
American Institute of Aeronautics and Astronautics
Reference22 articles.
1. A parallel, implicit, multi-dimensional upwind, residual distribution method for the Navier-Stokes equations on unstructured grids
2. Figure 13. Shock vortex interaction: pressure contours at t = 0:2 (left) and t = 0:4 (right); solution provided by the proposed implicit third-order scheme. steady flows, in: Innovative methods for numerical solution of partial differential equations. ed. byM. M. Hafez and J. J. Chattot (World Scientific Publishing Co. Inc., New Jersey2002) pp.305-333.
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