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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：47/0  |  Submit date：2024/04/15
Oblique detonation engine  ODE  Propulsive performance  Specific impulse  
Study on aerodynamic loads at the inlet's cowl lip induced by multiple shock-shock interferences 期刊论文
ACTA MECHANICA SINICA, 2024, 卷号: 40, 期号: 4, 页码: 12
Authors:  Lin MY(林明月);  Yang F(杨帆);  Hu ZM(胡宗民);  Han GL(韩桂来)
Favorite  |  View/Download：41/0  |  Submit date：2024/05/27
Shock waves  Shock-shock interaction  Theoretical analysis  Hysteresis  
Self-similar unstart characteristics of supersonic contraction duct with an expansion corner 期刊论文
PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 1, 页码: 20
Authors:  Tong XT(仝晓通);  Yue LJ(岳连捷);  Wu WN(邬婉楠);  Zhang QF(张启帆);  Chen H(陈昊)
Favorite  |  View/Download：72/0  |  Submit date：2024/03/11
Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:  Dai, Chunliang;  Sun, Bo;  Yue LJ(岳连捷);  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yu, Jianyi
Adobe PDF(5674Kb)  |  Favorite  |  View/Download：82/14  |  Submit date：2024/02/19
Scramjet inlet  Starting ability  Thermochemical  Work performance  
Similarity Analysis on Two-Dimensional Hypersonic Inlets Unstart 期刊论文
AIAA JOURNAL, 2023, 卷号: 61, 期号: 2, 页码: 555-572
Authors:  Tong XT(仝晓通);  Yue LJ(岳连捷);  Chen H(陈昊);  Zhang QF(张启帆);  He CM(何成明)
Adobe PDF(6058Kb)  |  Favorite  |  View/Download：196/56  |  Submit date：2022/11/28
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  Favorite  |  View/Download：351/102  |  Submit date：2022/08/23
Aerodynamic Coefficients  Two Stage to Orbit  Aerodynamic Performance  Hypersonic Flight  Hypersonic Wind Tunnels  Solenoid Valves  Oblique Shock  Pneumatic Actuator  Hypersonic Flows  Computer Aided Engineering  
Lagrange Optimization of Shock Waves for Two-Dimensional Hypersonic Inlet with Geometric Constraints 期刊论文
AEROSPACE, 2022, 卷号: 9, 期号: 10, 页码: 15
Authors:  Li YL(李育凌);  Yue LJ(岳连捷);  He CM(何成明);  Wu WN(邬婉楠);  Chen H(陈昊)
Adobe PDF(3520Kb)  |  Favorite  |  View/Download：301/91  |  Submit date：2022/11/14
scramjet inlet  Lagrange optimization method  shock configuration  
Experimental investigation of combustion-induced starting hysteresis in the scramjet 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 9, 页码: 96103
Authors:  Zhang QF(张启帆);  Chen H(陈昊);  Wu ZJ(吴振杰);  Gao ZB(高占彪);  Luo WH(罗苇航);  Gu HB(顾洪斌);  Yue LJ(岳连捷)
Adobe PDF(2852Kb)  |  Favorite  |  View/Download：179/60  |  Submit date：2022/10/23
Experimental Study of Kerosene Ignition and Flame Stabilization in a Supersonic Combustor 期刊论文
International Journal of Turbo & Jet-Engines, 2022, 卷号: 39, 期号: 3, 页码: 403-410
Authors:  Meng Y(孟宇);  Gu HB(顾洪斌);  Zhang XY(张新宇)
Adobe PDF(3187Kb)  |  Favorite  |  View/Download：319/97  |  Submit date：2021/10/29
Control of shock-wave/boundary-layer interaction using abackward-facing step 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 126, 页码: 13
Authors:  Zhai J;  Zhang CA(张陈安);  Wang FM(王发民);  Zhang WW(张伟为)
Adobe PDF(4533Kb)  |  Favorite  |  View/Download：213/58  |  Submit date：2022/12/20
Shock-wave/boundary-layer interaction  Backward-facing step  Flow separation  Hypersonic inlet