DNS of Transition To Turbulence in a Mach 6 Boundary Layer
Author:
Affiliation:
1. University of Minnesota, Minneapolis
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-3106
Reference26 articles.
1. Ground Test Studies of the HIFiRE-1 Transition Experiment Part 2: Computational Analysis
2. Compressible turbulent channel flows: DNS results and modelling
3. A numerical study of turbulent supersonic isothermal-wall channel flow
4. Direct numerical simulation of compressible turbulent channel flow between adiabatic and isothermal walls
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