Steady Turbulent Flow Computations Using a Low Mach Fully Compressible Scheme
Author:
Affiliation:
1. School of Engineering, Cranfield University, Cranfield MK43 0AL, United Kingdom
2. Ricardo Software, Shoreham-by-Sea, West Sussex BN43 5FG, United Kingdom
3. School of AMME, University of Sydney, Sydney, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052948
Reference54 articles.
1. Implementation of Preconditioned Dual-Time Procedures in OVERFLOW
2. On the behaviour of upwind schemes in the low Mach number limit
3. On the behavior of upwind schemes in the low Mach number limit: II. Godunov type schemes
4. Recent developments in the computation of compressible low Mach number flows
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