A detailed modelling on spray atomisation and combustion of LOX/GCH4 in variable area pintle injector rocket engines-Reference-Cited by-同舟云学术

A detailed modelling on spray atomisation and combustion of LOX/GCH4 in variable area pintle injector rocket engines

Published:2021-06-07 Issue:4 Volume:25 Page:718-750
ISSN:1364-7830
Container-title:Combustion Theory and Modelling
language:en
Short-container-title:Combustion Theory and Modelling

Author:

Radhakrishnan Kanmaniraja¹²,Lee Keonwoong¹³,Koo Jaye⁴

Affiliation:

1. Department of Aerospace and Mechanical Engineering, Graduate School of Korea Aerospace University, Goyang 10540, Republic of Korea

2. Department of Automotive Engineering, Korea National University of Transportation, Chungju, 27469, Republic of Korea

3. BK21 FOUR Smart Drone Convergence, Korea Aerospace University, Goyang 10540, Republic of Korea

4. School of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang, Republic of Korea

Funder

National Research Foundation of Korea

the Korean Government

Publisher

Informa UK Limited

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,Modelling and Simulation,General Chemical Engineering,General Chemistry

Link

https://www.tandfonline.com/doi/pdf/10.1080/13647830.2021.1937702

Reference70 articles.

1. H.W. Douglass, H.W. Schmidt, and L. Levinson, Liquid propellant gas generators, Tech. Rep. NASA SP–8081, 1972.

2. M.J.L. Turner, Rocket and Spacecraft Propulsion: Principles, Practice and New Developments, Springer-Verlag Berlin Heidelberg, New York, 2005, pp. 197–247.

3. Pintle Injectors

4. Effects of skip distance on the spray characteristics of a pintle injector

Cited by 7 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. Multi‒scale numerical investigations on the atomization performance of liquid‒liquid pintle injector;Aerospace Science and Technology;2024-11

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

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

4. NUMERICAL SIMULATIONS OF LIQUID FILM PRIMARY BREAKUP IN A PINTLE INJECTOR: A PARAMETRIC STUDY;Atomization and Sprays;2024

5. Experimental and Numerical Study on the Ablation Analysis of a Pintle Injector for GOX/GCH4 Rocket Engines;Coatings;2023-05-31