The effect of secondary boundary layer combustion of hydrogen on rocket plume heat release characteristics-Reference-Cited by-同舟云学术

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The effect of secondary boundary layer combustion of hydrogen on rocket plume heat release characteristics

Published:2024-06 Issue: Volume:71 Page:1174-1190
ISSN:0360-3199
Container-title:International Journal of Hydrogen Energy
language:en
Short-container-title:International Journal of Hydrogen Energy

Author:

Wang Limin,Cheng Qunli,Wang Jiannan,Zhang Yongwei,Zhang Weimeng,Liu Shuyuan,Xia Zhixun

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference31 articles.

1. Rocket exhaust plume phenomenology;Simmons,2000

2. Multi-phase reactive numerical simulations of a model solid rocket motor exhaust jet;Troyes,2006

3. Numerical investigation of twin-nozzle rocket plume phenomenology J Propul;Ebrahimi;Power,2000

4. Molecular gas dynamics and the direct simulation of gas flow;Bird,1994

5. A CFD/DSMC analysis of plumes and plume impingement during shuttle/Mir docking;Lumpkin,1995

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