Scaling of incipient separation in high speed laminar flows
Author:
Affiliation:
1. Iowa State University, Ames, Iowa 50010
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12356
Reference14 articles.
Cited by 5 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. Comparative studies of shock-wave boundary-layer interactions in Earth and Mars atmospheres;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-04-22
2. Incipient Separation in Laminar Ramp-Induced Shock-Wave/Boundary-Layer Interactions;AIAA Journal;2018-02
3. DSMC Computations of Separation over a `Tick' model in Hypersonic High Enthalpy Transitional Flows;55th AIAA Aerospace Sciences Meeting;2017-01-05
4. Numerical Study of Hypersonic Separated Flow over an Expansion-Compression Surface;20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2015-07-02
5. Theory of Local Heat Transfer in Shock/Laminar Boundary-Layer Interactions;Journal of Thermophysics and Heat Transfer;1998-07
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