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Combustion Hysteresis Phenomenon in a Dual-Mode Scramjet 期刊论文
AIAA JOURNAL, 2024, 页码: 14./通讯作者：Yao, Wei
作者:  Wang, Yu;  Yao W(姚卫);  Zhang, Zheng;  Liu, Jianwen
收藏  |  浏览/下载：14/0  |  提交时间：2025/01/13
Combustion hysteresis  Dual-mode scramjet  Hydrogen fuels  IDDES  
Supersonic Combustion Mode Analysis of a Cavity Based Scramjet 期刊论文
AEROSPACE, 2022, 卷号: 9, 期号: 12, 页码: 826./通讯作者：Chen, F (corresponding author), Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China., Gu, HB (corresponding author), Inst Mech CAS, Beijing 100190, Peoples R China.
作者:  Meng, Yu;  Sun WM(孙文明);  Gu HB(顾洪斌);  Chen, Fang;  Zhou RX(周芮旭)
Adobe PDF(3719Kb)  |  收藏  |  浏览/下载：97/22  |  提交时间：2023/04/20
scramjet  combustion mode  POD  instability  
Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11./通讯作者：Sun, Mingbo, Zhao, Guoyan
作者:  Liu, Mingjiang;  Sun, Mingbo;  Zhao, Guoyan;  Meng Y(孟宇);  Huang, Yuhui;  Ma, Guangwei;  Wang, Hongbo
Adobe PDF(3841Kb)  |  收藏  |  浏览/下载：204/45  |  提交时间：2022/12/20
Tandem-cavity  Scramjet combustor  Combustion mode  Thrust performance  
Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10./通讯作者：Yue, Lianjie
作者:  Zhang X(张旭);  Yue LJ(岳连捷);  Huang TL(黄庭隆);  Zhang QF(张启帆);  Zhang XY(张新宇)
浏览  |  Adobe PDF(3862Kb)  |  收藏  |  浏览/下载：426/142  |  提交时间：2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
Computational realization of multiple flame stabilization modes in DLR strut-injection hydrogen supersonic combustor 期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 卷号: 37, 期号: 3, 页码: 3685-3692./通讯作者：Yao, W, Zhang, P
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1820Kb)  |  收藏  |  浏览/下载：547/176  |  提交时间：2018/12/27
Supersonic combustion  Flame stabilization mode  DLR Strut injection scheme  Stagnation Temperature  Overall equivalence ratio  
Modeling Analysis on Cavity-based Flame Stabilization in Scramjet Combustor 会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
作者:  Wu K(吴坤);  Zhang P(张鹏);  Fan XJ(范学军)
收藏  |  浏览/下载：185/0  |  提交时间：2019/11/20
Combustion chemistry  Combustion dynamics  Dual  mode scramjet  Flame stabilization  Improved delayed detached eddy simulations  Overall reactions  Scramjet combustors  Shock  wave structures  
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
作者:  Wang ZP(王知溥);  Li F(李飞);  Gu HS;  Yu XL(余西龙);  Zhang XY(张新宇);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1112Kb)  |  收藏  |  浏览/下载：644/248  |  提交时间：2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas  
Study on Judgment Method of Combustion Mode on Dual-mode Scramjet 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
作者:  Chen Q(陈强);  Chen LH(陈立红);  Gu HB(顾洪斌);  Zhang XY(张新宇);  Wang P
浏览  |  Adobe PDF(759Kb)  |  收藏  |  浏览/下载：616/195  |  提交时间：2014/03/11
Combustion Mode  Scramjet  Artificial Neural Network