Transition Within a Hypervelocity Boundary Layer on a 5-Degree Half-Angle Cone in Air/CO2 Mixtures
Author:
Affiliation:
1. California Institute of Technology
2. Sandia National Laboratories
3. Air Force Research Laboratory
4. University of Minnesota, Minneapolis
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-523
Reference39 articles.
1. Hypersonic Flight Transition Data Analysis Using Parabolized Stability Equations with Chemistry Effects
2. 3Germain, P., The Boundary Layer on a Sharp Cone in High-Enthalphy Flow, Ph.D. thesis,California Institute of Technology, Pasadena, CA, 1993.
3. Enthalpy Effects on Hypervelocity Boundary-Layer Transition: Ground Test and Flight Data
4. Numerical study of hypersonic reacting boundary layer transition on cones
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