Effect of the recess length on the dynamic characteristics of liquid-centered swirl coaxial injectors-Reference-Cited by-同舟云学术

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Effect of the recess length on the dynamic characteristics of liquid-centered swirl coaxial injectors

Published:2022-10 Issue: Volume:199 Page:1-13
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Ahn Jonghyun^ORCID,Lim Hayoung,Jeong Gijeong,Ahn Kyubok^ORCID

Funder

Korea Aerospace Research Institute

National Research Foundation of Korea

NRF

Ministry of Science, ICT and Future Planning

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. Modern engineering for design of liquid-propellant rocket engines;Huzel,1992

2. LOX/GH2 shear coaxial injector atomization studies at large momentum flux ratios;Woodward,2006

3. Shear coaxial injector spray characterization near the LOX post tip region;Glogowski,1995

4. Aerodynamic instability and disintegration of inviscid liquid sheets;Clark;Proc. R. Soc. Lond. A. Math. Phys. Sci.,1972

Cited by 3 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. Investigation on spray and flame stabilization of a LOX/methane swirl coaxial injector;Combustion and Flame;2024-08

2. Non-circular pressure swirl nozzles injecting into stagnant air;International Journal of Multiphase Flow;2024-05

3. Numerical Study on the Self-Pulsation Characteristics of LOX/GH2 Swirl Coaxial Injector;International Journal of Aerospace Engineering;2024-03-15

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