Numerical study of combustion and cooling performance of a gaseous oxygen and gaseous methane rocket combustor with the needle-bolt injector-Reference-Cited by-同舟云学术

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Numerical study of combustion and cooling performance of a gaseous oxygen and gaseous methane rocket combustor with the needle-bolt injector

Published:2023-02 Issue: Volume:221 Page:119806
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Zhang G.D.,Li G.X.,Xing R.P.,Zhang Hu,Tang G.H.

Funder

Higher Education Discipline Innovation Project

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference33 articles.

1. Synergistic effect of a hybrid additive for hydrogen peroxide-based low toxicity hypergolic propellants;Kim;Combustion Flame,2021

2. Effect of metal additives on neutralization and characteristics of AP/HTPB solid propellants;Vellaisamy;Combustion Flame,2020

3. Numerical simulation of ammonium dinitramide (ADN)-based non-toxic aerospace propellant decomposition and combustion in a monopropellant thruster;Zhang;Energ. Conver. Manage.,2014

4. Gel propellants;Padwal;Prog. Energy Combust. Sci.,2021

5. LOX/methane reusable rocket propulsion at reach with large scale demonstrators tested;Boue;Acta Astronaut.,2018

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1. Guest Editorial: Special issue on the 8th Asian Symposium on Computational Heat Transfer and Fluid Flow (ASCHT 2021);Applied Thermal Engineering;2024-04

2. Study on the dynamic numerical simulation of flow and combustion in hybrid rocket motors based on a discrete phase model;Acta Astronautica;2024-02

3. Experimental and numerical study on liquid film cooling performance under heated wall condition;Applied Thermal Engineering;2024-02

4. Flame structure of GCH4/GOX pintle model combustor with wall confinement;Aerospace Science and Technology;2024-02

5. Numerical Study on the Combustion Characteristics of an Ammonia-Fueled Pintle Rocket Engine;2024

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