Analysis of Low-Frequency Unsteadiness in the Direct Numerical Simulation of a Shockwave and Turbulent Boundary Layer Interaction
Author:
Affiliation:
1. Princeton University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-3711
Reference23 articles.
1. Direct Numerical Simulation of Supersonic Turbulent Boundary Layer over a Compression Ramp
2. Correlation of separation shock motion with pressure fluctuations inthe incoming boundary layer
3. Megahertz Visualization of Compression-Corner Shock Structures
4. Analysis of shock motion in shockwave and turbulent boundary layer interaction using direct numerical simulation data
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