PSE analysis of reacting hypersonic boundary layer transition
Author:
Affiliation:
1. Minnesota, Univ.; U.S. Army, High Performance Computing Research Center, Minneapolis
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-3793
Reference28 articles.
1. Transition on a slender cone in hypervelocity flow
2. Enthalpy Effects on Hypervelocity Boundary-Layer Transition: Ground Test and Flight Data
3. Numerical study of hypersonic reacting boundary layer transition on cones
4. The solution of the Navier-Stokes equations using Gauss-Seidel line relaxation
5. M. J. Wright, G. V. Candler, and D. Bose. "A Data-Parallel Line-Relaxation Method for the Navier-Stokes Equations0022. APAA Paper No. 97-2046CP, June 1997.
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