Numerical Simulation of Hypersonic Boundary Layer Receptivity and Stability on Blunt Circular Cones-Reference-Cited by-同舟云学术

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Numerical Simulation of Hypersonic Boundary Layer Receptivity and Stability on Blunt Circular Cones

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
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Short-container-title:

Author:

Zhong Xiaolin¹

Affiliation:

1. University of California, Los Angeles

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-940

Reference40 articles.

1. Schneider, S.P., Hypersonic Laminar-Turbulent Transition on Circular Cones and Scramjet Forebodies. Progress inAerospaceSciences,2004.40: p.1-50.

2. Schneider, S.P., Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds. Journal of Spacecraft and Rockets,1999. 36(1): p.8-20.

3. Stetson, K.F., Rushton, G. H., Shock Tunnel Investigation of Boundary-Layer Transition at M = 5.5. AIAA JOURNAL,1967.5(5):p.899-906.

4. Stetson, K.F., Thompson, E. R., Donaldson, J. C., and Siler, L. G., Laminar Boundary Layer Stability Experimentsona ConeatMach8, Part2:BluntCone.1984.AIAApaper84-0006.

Cited by 1 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. Numerical Simulation of Nose Bluntness Effects on Hypersonic Boundary Layer Receptivity to Freestream Disturbances;41st AIAA Fluid Dynamics Conference and Exhibit;2011-06-14

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