Semi-Analytic Reconstruction of Flux in Finite Volume Formulations
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-1090
Reference26 articles.
1. Computational Fluid Dynamic Technology for Hypersonic Applications
2. Computational Aerothermodynamic Simulation Issues on Unstructured Grids
3. Towards the ultimate conservative difference scheme. V. A second-order sequel to Godunov's method
4. On Upstream Differencing and Godunov-Type Schemes for Hyperbolic Conservation Laws
5. Approximate Riemann solvers, parameter vectors, and difference schemes
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1. An unstructured solver for argon plasma flows with reduced state-to-state kinetics;44th AIAA Plasmadynamics and Lasers Conference;2013-06-22
2. Simple and Parameter-Free Second Slope Limiter for Unstructured Grid Aerodynamic Simulations;AIAA Journal;2012-06
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