Mach 10 Hypersonic Nozzle: Improved Flow Quality-Reference-Cited by-同舟云学术

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Mach 10 Hypersonic Nozzle: Improved Flow Quality

Published:2003-01 Issue:1 Volume:40 Page:126-131
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Lacey John¹,Inoue Yasutoshi²,Higashida Akio³,Inoue Manabu⁴,Ishizaka Kouichi⁵,Korte John J.⁶

Affiliation:

1. Aero Systems Engineering, St. Paul, Minnesota 55107

2. National Aerospace Laboratory, Tokyo 182-8522, Japan

3. Mitsubishi Heavy Industries, Ltd., Kobe 652-8585, Japan

4. Mitsubishi Heavy Industries, Ltd., Tokyo 100-8315, Japan

5. Mitsubishi Heavy Industries, Ltd., Takasago Hyogo 676-8686, Japan

6. NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/2.3925

Reference16 articles.

Cited by 2 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. Development of a Supersonic Aerodynamic Test Section Using Computational Modeling;39th AIAA Fluid Dynamics Conference;2009-06-14

2. Modern developments in hypersonic wind tunnels;The Aeronautical Journal;2006-01

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