Effects of Wall Cooling on Supersonic Modes in High- Enthalpy Hypersonic Boundary Layers over a Cone
Author:
Affiliation:
1. NASA Langley Research Center
2. National Institute of Aerospace
Publisher
American Institute of Aeronautics and Astronautics
Reference25 articles.
Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. On the role of discrete and continuous modes in a cooled high-speed boundary layer flow;Journal of Fluid Mechanics;2022-05-19
2. Secondary instability of Görtler vortices in hypersonic boundary layer over an axisymmetric configuration;Theoretical and Computational Fluid Dynamics;2022-01-28
3. 40 Years of Transition Research at NASA: A Personal Perspective;IUTAM Laminar-Turbulent Transition;2021-07-31
4. Parabolized Stability Analysis of Hypersonic Thermal–Chemical Nonequilibrium Boundary-Layer Flows;AIAA Journal;2021-07
5. Instabilities and transition in cooled wall hypersonic boundary layers;Journal of Fluid Mechanics;2021-03-11
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