Experimental and numerical investigations on flow field characteristics of pintle injector
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference29 articles.
1. Simulation of thrust control by fluidic injection and pintle in a solid rocket motor;Yan;Aerosp. Sci. Technol.,2020
2. Numerical investigation of flame appearance and heat flux and in a deep-throttling variable thrust rocket engine;Jin;Aerosp. Sci. Technol.,2019
3. Intermittent back-flash phenomenon of supersonic combustion in the staged-strut scramjet engine;Zhu;Aerosp. Sci. Technol.,2018
4. Influence of momentum ratio and its throttling method on spray characteristics of pintle injector;Chen;Acta Phys. Sin.,2019
5. Numerical study on the combustion characteristics of a fuel-centered pintle injector for methane rocket engines;Son;Acta Astronaut.,2017
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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. Experimental study on the droplet size distribution of radial orifice gas–liquid pintle injector at ambient pressure;Experimental Thermal and Fluid Science;2024-06
4. Spray characteristics of a multi-slit type throttleable pintle injector with different slit heights;Acta Astronautica;2024-02
5. NUMERICAL SIMULATIONS OF LIQUID FILM PRIMARY BREAKUP IN A PINTLE INJECTOR: A PARAMETRIC STUDY;Atomization and Sprays;2024
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