NASA NTRS · 19930062815
A multiblock, multigrid solution procedure for multielement airfoils
Abstract
A block-structured grid formulation is presented and discussed. The compressible Euler equations are solved on the decomposed domain with a multigrid method based on Runge-Kutta time stepping and centered spatial differencing. The flexibility of the multiblock approach is demonstrated by computing low speed inviscid flow over two different multielement airfoil configurations.
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Sanetrik, Mark D., Swanson, R. C.. 1991-05-01. A multiblock, multigrid solution procedure for multielement airfoils. https://ntrs.nasa.gov/citations/19930062815
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