Effect of injection conditions on mixing performance of pintle injector for liquid rocket engines-Reference-Cited by-同舟云学术

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Effect of injection conditions on mixing performance of pintle injector for liquid rocket engines

Published:2018-09 Issue: Volume:150 Page:105-116
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Radhakrishnan Kanmaniraja,Son Min,Lee Keonwoong,Koo Jaye

Funder

Agency for Defense Development

Advanced Research Center Program

National Research Foundation of Korea(NRF)

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference23 articles.

1. Supercomputer predictive modeling for ensuring space flight safety;Betelin;Acta Astronaut.,2015

2. Accumulation of errors in numerical simulations of chemically reacting gas dynamics;Smirnov;Acta Astronaut.,2015

3. Detonation engine fed by acetylene–oxygen mixture;Smirnov;Acta Astronaut.,2014

4. Combustion onset in non -uniform dispersed mixtures;Smirnov;Acta Astronaut.,2015

5. Evaporation and ignition of droplets in combustion chambers modeling and simulation;Betelin;Acta Astronaut.,2012

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1. Effects of slit geometric parameters on spray characteristics of double-slit pintle injectors;Experimental Thermal and Fluid Science;2025-01

2. Multi‒scale numerical investigations on the atomization performance of liquid‒liquid pintle injector;Aerospace Science and Technology;2024-11

3. Research on performance seeking control of turbofan engine in minimum hot spot temperature mode;International Journal of Turbo & Jet-Engines;2024-06-17

4. Experimental study on the droplet size distribution of radial orifice gas–liquid pintle injector at ambient pressure;Experimental Thermal and Fluid Science;2024-06

5. Impact of chemical modeling on the numerical analysis of a LOx/GCH4 rocket engine pintle injector;Acta Astronautica;2024-05

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