Characteristics of spray and combustion in gas-centered swirl coaxial injector with varying gas nozzle diameter-Reference-Cited by-同舟云学术

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Characteristics of spray and combustion in gas-centered swirl coaxial injector with varying gas nozzle diameter

Published:2024-02 Issue: Volume:215 Page:631-641
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Lee Jungho^ORCID,Woo Seongphil,Lee Ingyu^ORCID,Han Yeoungmin,Yoon Youngbin^ORCID

Funder

Institute of Advanced Aerospace Technology, Seoul National University

Korea Aerospace Research Institute

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. History of Liquid Propellant Rocket Engines;Sutton,2005

2. Space Propulsion Analysis and Design;Humble,1995

3. Modern Engineering for Design of Liquid-Propellant Rocket Engines;Huzel,1992

4. Rocket Propulsion Elements;Sutton,2001

5. Modern Liquid Propellant Rocket Engines;Zandbergen,2000

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. Effects of injector spacing and momentum flux ratio on combustion instability in a model chamber with gas-centered swirl coaxial injectors;Aerospace Science and Technology;2024-11

2. Investigation of the oxygen-methane combustion and heating characteristics in industrial-scale copper anode refining furnace;Energy;2024-07

3. Experimental Study of Spray and Combustion Characteristics in Gas-Centered Swirl Coaxial Injectors: Influence of Recess Ratio and Gas Swirl;Aerospace;2024-03-08

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