BOUNDARY-LAYER TRANSITION ON A HIGHLY COOLED 10 DEGREE CONE IN HYPERSONIC FLOWS-Reference-Cited by-同舟云学术

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BOUNDARY-LAYER TRANSITION ON A HIGHLY COOLED 10 DEGREE CONE IN HYPERSONIC FLOWS

Published:1964-08-16 Issue: Volume: Page:
ISSN:
Container-title:Entry Technology Conference
language:
Short-container-title:

Author:

NAGAMATSU HENRY¹,SHEER RUSSELL¹

Affiliation:

1. GENERAL ELECTRIC RESEARCH LAB, SCHENECTADY, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1964-1312

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. Flight test measurements of boundary-layer transition on a nonablating 22 deg cone;Journal of Spacecraft and Rockets;1970-02

2. Flight test measurements of boundary-layer transition on a nonablating 22 deg cone;Entry Vehicle Systems and Technology Meeting;1968-08-16

3. Shock tunnel investigation of boundary-layer transition at M equals 5.5.;AIAA Journal;1967-05

4. Numerical treatment of turbulent flows;AIAA Journal;1965-07

5. Exploratory hypersonic boundary-layer transition studies;AIAA Journal;1965-07

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