Extensions Of A Rapid Engineering Approach to Modeling Hypersonic Laminar To Turbulent Transitional Flows
Author:
Affiliation:
1. CRAFT Tech
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-892
Reference36 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. Experimental studies of shock wave/wall jet interaction in hypersonic flow
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2. Modern Approaches for Calculating Flow Parameters during a Laminar–Turbulent Transition in a Boundary Layer;High Temperature;2018-01
3. RANS modeling of high-speed aerodynamic flow transition with consideration of stability theory;Progress in Aerospace Sciences;2013-04
4. Modeling Hypersonic Laminar to Turbulent Transitional Flows for 3D Geometries Using a Two-Equation Onset and Intermittency Transport Models;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09
5. Development of an Intermittency Equation for the Modeling of the Supersonic/Hypersonic Boundary Layer Flow Transition;Flow, Turbulence and Combustion;2011-03-01
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