Numerical Investigation of Supersonic Transition for a Circular Cone at Mach 3.5
Author:
Affiliation:
1. The University of Arizona
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-4397
Reference29 articles.
1. Numerical Simulations of Laminar-Turbulent Transition In Supersonic Boundary Layer
2. Investigation of Oblique Breakdown in a Supersonic Boundary Layer at Mach 2 Using DNS
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