Numerical study of injection strategy based on cavity combustor under oblique shock wave interference-Reference-Cited by-同舟云学术

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Numerical study of injection strategy based on cavity combustor under oblique shock wave interference

Published:2022-10 Issue:86 Volume:47 Page:36693-36702
ISSN:0360-3199
Container-title:International Journal of Hydrogen Energy
language:en
Short-container-title:International Journal of Hydrogen Energy

Author:

Zuo Qiuru,Yu Huanli,Dai Jian^ORCID,Yan Yude,Chen Long

Publisher

Elsevier BV

Subject

Energy Engineering and Power Technology,Condensed Matter Physics,Fuel Technology,Renewable Energy, Sustainability and the Environment

Reference49 articles.

1. Experimental study of cone-struts and cavity flameholders in a kerosene-fueled round scramjet combustor;Zhang;Acta Astronaut,2017

2. Detonation engine fed by acetylene-oxygen mixture;Smirnov;Acta Astronaut,2014

3. Injection of multi hydrogen jets within cavity flame holder at supersonic flow;Edalatpour;Int J Hydrogen Energy,2019

4. Computational study of the cavity flow over sharp nose cone in supersonic flow;Pish;Int J Mod Phys C,2020

5. Hydrogen fuel in scramjet engines - a brief review;Choubey;Int J Hydrogen Energy,2020

Cited by 2 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. Flame stabilization and combustion enhancement in a scramjet combustor by varying strut injection angles;Archives of Thermodynamics;2024-07-12

2. Numerical Simulations of Hydrogen Leakage and Diffusion Behaviors in a Fuel Cell Ship;2024

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