A Rapid Engineering Approach to Modeling Hypersonic Laminar to Turbulent Transitional Flows for 2D and 3D Geometries
Author:
Affiliation:
1. Combustion Research and Flow Technology, Inc
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2600
Reference40 articles.
1. The Langley Stability and Transition Analysis Codes (LASTRAC) : LST, Linear & Nonlinear PSE for 2D, Axisymmetric, and Infinite Swept Wing Boundary Layers
2. Hypersonic Stability and Transition Experiments on Blunt Cones and a Generic Scramjet Forebody
3. Boundary Layer Transition on Slender Cones in Conventional and Low Disturbance Mach 6 Wind Tunnels
4. Experimental studies of shock wave/wall jet interaction in hypersonic flow
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