A Wide-range single engine: operated from startup to hypersonic condition-Reference-Cited by-同舟云学术

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A Wide-range single engine: operated from startup to hypersonic condition

Published:2011-04-11 Issue: Volume: Page:
ISSN:
Container-title:17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Naitoh Ken¹,Nakamura Kazushi¹,Emoto Takehiro¹

Affiliation:

1. Waseda University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2316

Reference1 articles.

1. Power for a Space Plane

Cited by 4 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. Weakly-pulsated center combustion engine: resulting in nearly-complete air-insulation effect caused by wall reflection of pressure-wave;AIAA Propulsion and Energy 2019 Forum;2019-08-16

2. High Thrust Measured for Pulsed Engine Based on Supermulti-jets Colliding;2018 Joint Propulsion Conference;2018-07-08

3. Computational experiments for improving the performance of Fugine based on supermulti-jets colliding working for a wide range of speeds from startup to hypersonic condition;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22

4. Fugine cycle theory: predicting high efficiency of the supermultijet-convergence engine working from startup to hypersonic scram mode;45th AIAA Thermophysics Conference;2015-06-18

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