Effect of gas injection holes on mixing and combustion in solid propellant ducted rockets-Reference-Cited by-同舟云学术

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Effect of gas injection holes on mixing and combustion in solid propellant ducted rockets

Published:2023-05 Issue: Volume:226 Page:120212
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Zhang Yiqiao,Wu Zhiwen,Zhang Zhihui,Chen Pengxin,Niu Yupeng,Chen Xiaodong,He Yongpan,Fang Guanlin

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference49 articles.

1. History of the development of solid rocket propellant in France;Davenas;J Propul Power,1995

2. A century of ramjet propulsion technology evolution;Fry;J Propul Power,2004

3. History of U.S. navy ramjet, scramjet, and mixed-cycle propulsion development;Waltrup;J Propul Power,2002

4. R. Stechman, R. Allen, History of ramjet propulsion development at the Marquardt company - 1944 to 1970, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Tucson, Arizona, AIAA Paper 2005-3538. https://doi.10.2514/6.2005-3538.

5. R. Fry, The U.S. navy’s contributions to airbreathing missile propulsion technology, AIAA Centennial of Naval Aviation Forum “100 Years of Achievement and Progress,” Virginia Beach, VA, AIAA Paper 2011-6942. https://doi.10.2514/6.2011-6942.

Cited by 3 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. Numerical study on the effect of multi-hole injector on three-dimensional flow and heat transfer properties of a novel combined solid rocket motor;International Journal of Thermal Sciences;2024-06

2. Effect of synergistic impact gas injection device on secondary combustion in boron-based ducted rockets;Applied Thermal Engineering;2024-04

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

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