Supersonic flux-split procedure for second moments of turbulence
Author:
Affiliation:
1. State University of New York at Stony Brook, Stony Brook, New York 11794-2300
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12544
Reference46 articles.
1. Numerical Investigation of Subsonic and Supersonic Asymmetric Vortical Flow
2. Turbulence modeling for complex hypersonic flows
3. Study of turbulence on supersonic compression surfaces using Reynolds stress model
4. Application of a Reynolds stress turbulence model to the compressible shear layer
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