NASA NTRS · 19900032628
Upwind control volumes - A new upwind approach
Abstract
This paper presents a new algorithm for the solution of the steady Euler equations in two-dimensional flow. It uses an upwind control volume approach in which a standard flux residual on triangular cells is distributed with a downwind bias. The resulting scheme is second order accurate on unstructured triangular meshes and produces sharp shocks without the addition of any shock smoothing. Results demonstrate its performance on a standard AGARD test case using both smooth and irregular unstructured meshes.
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Giles, Michael, Anderson, W. Kyle, Roberts, Thomas W.. 1990-01-01. Upwind control volumes - A new upwind approach. https://ntrs.nasa.gov/citations/19900032628
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