A Comparative Study of Gradient Reconstruction Methods for Unstructured Meshes with Application to Turbomachinery Flows
Author:
Affiliation:
1. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0069
Reference5 articles.
1. Towards Excellence in Turbomachinery CFD: A Hybrid Structured-Unstructured RANS Solver
2. Accurate and Efficient Discretization of Navier-Stokes Equations on Mixed Grids
3. A 3-D upwind Euler solver for unstructured meshes
4. Behavior of linear reconstruction techniques on unstructured meshes
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