Improving Low-Frequency Characteristics of Recycling/Rescaling Inflow Turbulence Generation
Author:
Affiliation:
1. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050705
Reference39 articles.
1. Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow
2. Oblique Shock Impinging on a Turbulent Boundary Layer: Low-Frequency Mechanisms.
3. Large-eddy simulation of low-frequency unsteadiness in a turbulent shock-induced separation bubble
4. Direct numerical simulation of impinging shock wave/turbulent boundary layer interaction at M=2.25
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