Spray patterns of multi-element swirl coaxial injector of interacting spray under different injection conditions
Author:
Affiliation:
1. Steelmaking Process Research Team, Hyundai Steel Company, Dangjin 31719, Republic of Korea
2. School of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 10540, Republic of Korea
Funder
National Research Foundation of Korea
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0058107
Reference32 articles.
1. History of Liquid Propellant Rocket Engines in the United States
2. Dynamics and stability of lean-premixed swirl-stabilized combustion
3. D. Preclik and P. Spagna, Low frequency and high frequency combustion oscillation phenomena inside a rocket combustion chamber fed by liquid or gaseous propellants AGARD, combustion instabilities in liquid-fueled propulsion systems, 1989.
4. Supercritical combustion of gas-centered liquid-swirl coaxial injectors for staged-combustion engines
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