Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-10 of 184 Help

Filters    
Selected(0)Clear Items/Page:    Sort:
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
基于主动射流控制的高超声速进气道再起动性能研究（英文） 期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:  靳一超;  姚卫
Adobe PDF(1844Kb)  |  Favorite  |  View/Download：194/47  |  Submit date：2023/02/09
高超声速进气道  不起动  再起动  主动射流  流动控制  
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  
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