Hybrid Reynolds-Averaged Navier-Stokes/Large-Eddy Simulations of Supersonic Turbulent Mixing
Author:
Affiliation:
1. NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135
2. Case Western Reserve University, Cleveland, Ohio 44106
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1934
Reference28 articles.
1. Assessment of Parameters Influencing the Prediction of Shear-Layer Mixing
2. A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields
3. Strategies for turbulence modelling and simulations
4. The effect of initial conditions on the development of a free shear layer
5. Growth of the two-dimensional mixing layer from a turbulent and nonturbulent boundary layer
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