Impact of Vibrational Nonequilibrium on the Supersonic Mode in Hypersonic Boundary Layers
Author:
Affiliation:
1. Lawrence Livermore National Laboratory, Livermore, California 94550
2. University of California, Los Angeles, Los Angeles, California 9009
Funder
Lawrence Livermore National Laboratory
Office of Naval Research
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058758
Reference47 articles.
1. Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers
2. Transition and Stability of High-Speed Boundary Layers
3. MackL. M. “Boundary Layer Linear Stability Theory,” AGARD Rept. 709, 1984.
4. Asymptotic analysis of inviscid perturbations in a supersonic boundary layer
5. Hypersonic viscous flow over a slender cone. III - Laminar instability and transition
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