Theoretical and Experimental Study of the Dynamics of a Liquid Swirl Injector-Reference-Cited by-同舟云学术

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Theoretical and Experimental Study of the Dynamics of a Liquid Swirl Injector

Published:2010-01 Issue:1 Volume:26 Page:94-101
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Fu Qing-fei¹,Yang Li-jun¹,Wang Xiang-dong¹

Affiliation:

1. Beijing University of Aeronautics and Astronautics, 100191 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.44271

Reference19 articles.

1. Liquid-Propellant Rocket Engine Injector Dynamics

Cited by 45 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. An Improved Comprehensive Atomization Model for Pressure Swirl Atomizers;Aerospace;2024-08-12

2. Experimental study of Cryogenic jet injection using centrifugal nozzles at supercritical pressure;Acta Astronautica;2024-08

3. Experimental study on the surface wave mode of a liquid film under the coupling effect of acoustic oscillation and electric field;Physics of Fluids;2024-03-01

4. Effect of inlet mass flow rate oscillation on simplex swirl injector flow based on VOF-to-DPM model;Acta Astronautica;2023-10

5. Spray combustion characteristics of a gas–liquid pintle injector with variable swirl intensities;Physics of Fluids;2023-09-01

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