Mach 6 Test of a Scramjet Engine with Multi-Staged Fuel Injection-Reference-Cited by-同舟云学术

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Mach 6 Test of a Scramjet Engine with Multi-Staged Fuel Injection

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Ueda Shuichi¹,Tomioka Sadatake¹,Ono Fumiei¹,Sakuranaka Noboru¹,Tani Kouichiro¹,Murakami Atsuo¹

Affiliation:

1. Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-1027

Reference17 articles.

1. Mach 8 Testing of a Scramjet Engine Model

Cited by 11 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. Experimental study of hysteresis and catastrophe in a cavity-based scramjet combustor;Chinese Journal of Aeronautics;2021-09

2. Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator;Chinese Journal of Aeronautics;2020-12

3. Fuel Distribution Depending on Internal Flow Separation in a Scramjet Engine;23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2020-03-10

4. Fluid Transport brought by a Strut-Cowl System in a Scramjet Engine;49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2013-07-12

5. Aerodynamic Effect brought by a Strut-Cowl System in a Scramjet Engine;18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference;2012-09-24

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