Simulation and Modeling of Hypersonic Turbulent Boundary Layers Subject to Favorable Pressure Gradients due to Streamline Curvature
Author:
Affiliation:
1. Ohio State University
2. NASA Langley Research Center
3. Texas A&M University
Publisher
American Institute of Aeronautics and Astronautics
Reference66 articles.
1. Response of a hypersonic turbulent boundary layer to favourable pressure gradients
2. The analogy between streamline curvature and buoyancy in turbulent shear flow
3. The effect of mean compression or dilatation on the turbulence structure of supersonic boundary layers
4. Structures in turbulent boundary layers subjected to adverse pressure gradients
5. Assessment of direct numerical simulation data of turbulent boundary layers
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