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Direct thrust test and asymmetric performance of porous ionic liquid electrospray thruster 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 4, 页码: 120-133./通讯作者：Wu, ZW
Authors:  Guo, Yuntao;  Sun, Wei;  Sun, Zhenning;  Wu, Zhiwen;  He JW(贺建武);  Yang C(杨超);  Wang, Ningfei
Adobe PDF(3342Kb)  |  Favorite  |  View/Download：155/47  |  Submit date：2023/06/15
Asymmetric performance  Direct thrust test  Ionic liquid electrospray thruster  Time of flight mass spec-trometry  Torsional thrust stand  
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
Authors:  Liu, Mingjiang;  Sun, Mingbo;  Zhao, Guoyan;  Meng Y(孟宇);  Huang, Yuhui;  Ma, Guangwei;  Wang, Hongbo
Adobe PDF(3841Kb)  |  Favorite  |  View/Download：250/83  |  Submit date：2022/12/20
Tandem-cavity  Scramjet combustor  Combustion mode  Thrust performance  
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1162Kb)  |  Favorite  |  View/Download：473/150  |  Submit date：2016/09/14
Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm