Experimental study on the spray characteristics of a pintle injector element-Reference-Cited by-同舟云学术

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Experimental study on the spray characteristics of a pintle injector element

Published:2022-05 Issue: Volume:194 Page:255-262
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Zhou Rui^ORCID,Shen Chibing

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. History of liquid propellant rocket engines in the United States;Sutton;J. Propul. Power,2003

2. Liquid propellant rocket engine throttling: a comprehensive review;Casiano;J. Propul. Power,2010

3. Comparison of blockage performance of pressure wave in structural baffle injector and fluidic baffle injector;Song;Acta Astronaut.,2020

4. Dynamic behavior of jet-swirl spray under resonance condition with external excitation;Jo;Acta Astronaut.,2021

5. Effect of self-excited instability on single liquid swirl injector flow characteristics;Jeong;Acta Astronaut.,2021

Cited by 15 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 slit geometric parameters on spray characteristics of double-slit pintle injectors;Experimental Thermal and Fluid Science;2025-01

2. Performance evaluation of modified pintle-type fuel injector for LRE (liquid rocket engine);Physics of Fluids;2024-05-01

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

4. Spray characteristics of a multi-slit type throttleable pintle injector with different slit heights;Acta Astronautica;2024-02

5. Pintle Injector Performance Sensitivity to the Radial Injection Arrangement;AIAA SCITECH 2024 Forum;2024-01-04

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