Influence of Favorable Pressure Gradients on a Mach 5.0 Turbulent Boundary Layer
Author:
Affiliation:
1. Physics, Materials and Applied Mathematics, LLC.
2. Texas A&M University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-748
Reference31 articles.
1. High-Speed Free Shear Layers with Molecular Non-Equilibrium: An Example of the Fluids Information Triad (Invited)
2. Anderson, J.,Hypersonic and High Temperature Gasdynamics,AIAA EducationSeries, DC,1989.
3. Hinze, J.,Turbulence, McGraw-Hill, New York, 1975.
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