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Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
Authors:  Yuan CK(苑朝凯);  Jiang ZL(姜宗林)
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Hypersonics  Shock tunnels  Flow characteristics  
Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
Authors:  Wang Q(汪球);  Luo K(罗凯);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟)
Adobe PDF(2057Kb)  |  Favorite  |  View/Download：264/82  |  Submit date：2020/08/26
Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow  
Transmission characteristics of EM wave in a finite thickness plasma 期刊论文
ACTA MECHANICA SINICA, 2013, 卷号: 29, 期号: 2, 页码: 189-195
Authors:  Zhu NY(竺乃宜);  Huang LS(黄立舜);  Wu B(吴彬);  Yu XL(余西龙);  Wu RH;  Meng G;  Ren AM;  Hu XT;  Wu B(吴彬)
Adobe PDF(770Kb)  |  Favorite  |  View/Download：950/244  |  Submit date：2013/06/13
Plasma  Electromagnetic Wave  Shock Tube  Numerical Simulation  
Numerical Study on Critical Wedge Angle of Cellular Detonation Reflections 期刊论文
Chinese Physics Letters, 2010, 卷号: 27, 期号: 2, 页码: 024701
Authors:  Wang G(王刚);  Zhang DL(张德良);  Liu KX(刘凯欣);  Liu KX
View  |  Adobe PDF(2000Kb)  |  Favorite  |  View/Download：1064/376  |  Submit date：2010/05/21