Towards High-Order Boundary Procedures for Finite-Volume and Finite-Difference Schemes
Author:
Affiliation:
1. National Institute of Aerospace
2. University of Michigan
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-1605
Reference18 articles.
1. Development of Vertex-Centered High-Order Schemes and Implementation in FUN3D
2. L2Roe: a low dissipation version of Roe's approximate Riemann solver for low Mach numbers
3. Third-Order Edge-Based Scheme for Unsteady Problems
4. Towards the ultimate understanding of MUSCL: Pitfalls in achieving third-order accuracy
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