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Study on the propulsive performance of oblique detonation engine 期刊论文
ENERGY, 2024, 卷号: 292, 页码: 11
Authors:  Liu YF(刘云峰);  Han, Xin;  Zhang, Zijian
Favorite  |  View/Download：38/0  |  Submit date：2024/04/15
Oblique detonation engine  ODE  Propulsive performance  Specific impulse  
Experimental investigation of mode transition process in a cavity-based scramjet 期刊论文
PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 4, 页码: 11
Authors:  Meng Y(孟宇);  Sun WM(孙文明);  Gu HB(顾洪斌);  Chen, Fang
Favorite  |  View/Download：13/0  |  Submit date：2024/05/14
Standing oblique detonation for hypersonic propulsion: A review 期刊论文
PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17
Authors:  Jiang ZL(姜宗林)
Adobe PDF(10386Kb)  |  Favorite  |  View/Download：62/7  |  Submit date：2024/02/26
Standing oblique detonation  Scramjet engine  Oblique detonation engine  Shock wave  Supersonic combustion  Hypersonic ramjet propulsion  
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023, 页码: 18
Authors:  Yao W(姚卫);  Liu H(刘杭);  Zhang Z(张政);  Zhang X(张旭);  Yue LJ(岳连捷);  Zhang XY(张晓源);  Li JP(李进平)
Adobe PDF(689Kb)  |  Favorite  |  View/Download：201/2  |  Submit date：2023/02/27
Experimental study of the high-power laser resistance of ablative material-filled sandwich panels with truss cores under hypersonic airflow 期刊论文
COMPOSITE STRUCTURES, 2022, 卷号: 301, 页码: 116139
Authors:  Yuan W(袁武);  Wang JT(王江涛);  Wang RX(王睿星);  Wang Z(王喆);  Song HW(宋宏伟);  Huang CG(黄晨光)
Adobe PDF(9765Kb)  |  Favorite  |  View/Download：196/54  |  Submit date：2022/10/23
Sandwich panel  Thermal insulation  Lightweight structure  Failure point  
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
Authors:  Liu, Mingjiang;  Sun, Mingbo;  Zhao, Guoyan;  Meng Y(孟宇);  Huang, Yuhui;  Ma, Guangwei;  Wang, Hongbo
Adobe PDF(3841Kb)  |  Favorite  |  View/Download：118/26  |  Submit date：2022/12/20
Tandem-cavity  Scramjet combustor  Combustion mode  Thrust performance  
Ram to scram mode transition in a simulated flight acceleration 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 6, 页码: 16
Authors:  Zhou RX(周芮旭);  Meng FZ(孟凡钊);  Li,Tuo;  Li ZP(李忠朋);  Lian H(连欢)
Adobe PDF(5582Kb)  |  Favorite  |  View/Download：192/33  |  Submit date：2022/09/16
Experimental Investigation of Abrupt Change in a Scramjet with Variable Mach-Number Flow 期刊论文
AIAA JOURNAL, 2022, 页码: 9
Authors:  Wu ZJ(吴振杰);  Zhang QF(张启帆);  Zhang X(张旭);  Luo WH(罗苇航);  Gao ZB(高占彪);  Yue LJ(岳连捷)
Adobe PDF(3049Kb)  |  Favorite  |  View/Download：169/28  |  Submit date：2022/07/18
Mechanisms of the destabilized Mach reflection of inviscid oblique detonation waves before an expansion corner 期刊论文
JOURNAL OF FLUID MECHANICS, 2022, 卷号: 940, 页码: 39
Authors:  Zhang, Zijian;  Liu YF(刘云峰);  Wen, Chihyung
Adobe PDF(1777Kb)  |  Favorite  |  View/Download：177/46  |  Submit date：2022/05/17
detonation waves  
Improved delayed detached eddy simulation of supersonic combustion fueled by liquid kerosene 期刊论文
FUEL, 2022, 卷号: 313, 页码: 13
Authors:  Shen, Wubingyi;  Huang, Yue;  Yao W(姚卫);  Liu, Hedong;  You, Yancheng
Adobe PDF(9915Kb)  |  Favorite  |  View/Download：187/44  |  Submit date：2022/05/17
Improved delayed detached eddy simulation  Liquid kerosene  Skeletal reaction mechanism  Equivalence ratio  Cavity-based scramjet combustor  Supersonic combustion