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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
作者:  Guo, Yuntao;  Sun, Wei;  Sun, Zhenning;  Wu, Zhiwen;  He JW(贺建武);  Yang C(杨超);  Wang, Ningfei
Adobe PDF(3342Kb)  |  收藏  |  浏览/下载:47/0  |  提交时间:2023/06/15
Asymmetric performance  Direct thrust test  Ionic liquid electrospray thruster  Time of flight mass spec-trometry  Torsional thrust stand  
On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
作者:  Jiang ZL(姜宗林);  Li JP(李进平);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Yu HR(俞鸿儒)
Adobe PDF(1090Kb)  |  收藏  |  浏览/下载:263/101  |  提交时间:2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities