Supercritical Fluid Dynamics of Pressure Swirl Injector with External Excitations-Reference-Cited by-同舟云学术

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Supercritical Fluid Dynamics of Pressure Swirl Injector with External Excitations

Published:2007-07-08 Issue: Volume: Page:
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Container-title:43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Zong Nan,Yang Vigor

Publisher

American Institute of Aeronautics and Astronautics

Reference26 articles.

1. Liquid-Propellant Rocket Engine Injector Dynamics

2. A.R. Jones, "Design optimization of a large pressure-jet atomizer for power plant," Proceeding of the 2ndinternation conferenceonliquid atomization andsprays,Madison,Wisconsin,1982.

Cited by 7 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. High-Pressure Experiments Relevant to Rocket Propulsion;High-Pressure Flows for Propulsion Applications;2020-01

2. The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine;Aerospace Science and Technology;2017-11

3. Analysis of Self-Excited Combustion Instabilities Using Decomposition Techniques;AIAA Journal;2016-09

4. Combustion behaviors of GO2/GH2 swirl-coaxial injector using non-intrusive optical diagnostics;Acta Astronautica;2016-06

5. Exploration of POD-Galerkin Method in Developing a Flame Model for Combustion Instability Problems;7th AIAA Theoretical Fluid Mechanics Conference;2014-06-13

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