Visualization of Flames in Combustion Chamber of Swirling-Oxidizer-Flow-Type Hybrid Rocket Engines-Reference-Cited by-同舟云学术

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Visualization of Flames in Combustion Chamber of Swirling-Oxidizer-Flow-Type Hybrid Rocket Engines

Published:2010-07-25 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Masugi Miho,Ide Tatsuya,Sakurai Takashi,Yuasa Saburo,Shiraishi Noriko,Shimada Toru

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. Fundamentals of Hybrid Boundary-Layer Combustion

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. Ignition processes and characteristics of charring conductive polymers with a cavity geometry in precombustion chamber for applications in micro/nano satellite hybrid rocket motors;Defence Technology;2023-05

2. Experimental and numerical investigation of swirling H2O2 and polypropylene hybrid rocket motor with regenerative cooling;Acta Astronautica;2022-01

3. The "Vortex Reloaded" project: experimental investigation on fully tangential vortex injection in N2O - paraffin hybrid motors;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30

4. Numerical and Experimental Investigation on Vortex Injection in Hybrid Rocket Motors;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

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