High-Order Meshes for Flow Simulations with a Spectral Difference Method
Author:
Affiliation:
1. Technological Institute of Aeronautics (ITA)
2. Aeronautics and Space Institute (IAE)
3. University of Kansas, Lawrence
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4294
Reference37 articles.
1. A High-Order Accurate Discontinuous Finite Element Method for the Numerical Solution of the Compressible Navier–Stokes Equations
2. High order boundary treatment for high order methods in computational fluid dynamics
3. A Study of Curved Boundary Representations for 2D High Order Euler Solvers
4. Implicit Spectral Difference Method Solutions of Compressible Flows Considering High-Order Meshes
5. From Electrostatics to Almost Optimal Nodal Sets for Polynomial Interpolation in a Simplex
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