Improved Flux Formulations for Unsteady Low Mach Number Flows
Author:
Affiliation:
1. Combustion Research and Flow Technology
2. Air Force Research Lab (AFRL), Space and Missile Propulsion Divison
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-3067
Reference15 articles.
1. PRECONDITIONING TECHNIQUES IN COMPUTATIONAL FLUID DYNAMICS
2. High-resolution viscous flow simulations at arbitrary Mach number
3. A sequel to AUSM, Part II: AUSM+-up for all speeds
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