Analysis of Laminar-Turbulent Transition in Hypersonic Flight Using PSE-Chem
Author:
Affiliation:
1. University of Minnesota
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3057
Reference27 articles.
1. Determination of spatial amplification factors and their applicationto predicting transition
2. Boundary-layer transition on a cone and flat plate at Mach 3.5
3. Hypersonic Flight Transition Data Analysis Using Parabolized Stability Equations with Chemistry Effects
4. 5M.R.Malik, R.E. Spall, and C.L.Chang. “Effect of Nose Bluntness on Boundary Layer Stability and Transition”. AIAA Paper No. 90-0112, January 1990.
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