Measurement on Transition of Hypersonic Boundary Layer Over Circular Cone-Reference-Cited by-同舟云学术

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Measurement on Transition of Hypersonic Boundary Layer Over Circular Cone

Published:2007-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
language:
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Author:

Bi Zhixian¹,Zhu Nanji¹,Shen Qing¹,Zhang Zhanfeng¹

Affiliation:

1. China Acadamy of Aerospace Aerodynamic

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-6728

Reference26 articles.

1. 1N.W.Sheetz,Jr.,Free-flightboundarylayertransitioninvestigationsathypersonicspeeds,AIAApaper65-127,1965.

2. Ground test facilities for aerothermal and aero-optical evaluation of hypersonic interceptors

3. The search for optimum configurations for re-entry vehicles

4. 5Kenneth F. Stetson, "Effect of Bluntness and Angle of Attack on Boundary Layer Transition on Cones and Biconic Configurations". AIAA 79-0269.

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. An Interferential Streak Instability of Boundary Layer over a Cone at Mach 6;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

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