NASA NTRS · 19840035089
Multigrid solution of the Euler equations for aircraft configurations
Abstract
A multigrid scheme for solving the Euler equations is presented. The method has been successfully applied to two-dimensional airfoil calculations on both O-type and C-type meshes. In three dimensions the scheme has proved equally effective and calclations of flows over wing/body combinations are possible with convergence achieved in less than 100 cycles.
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Jameson, A., Baker, T. J.. 1984-01-01. Multigrid solution of the Euler equations for aircraft configurations. https://ntrs.nasa.gov/citations/19840035089
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