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Parameters for evaluating the efficiency of inlet compression 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors:  Chen KT(陈科挺);  Yue LJ(岳连捷);  Zhang XY(张新宇)
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Airbreathing engine  Compression efficiency  Compression quality  Inlet  Self-consistency  
高速进气道低马赫数不起动特性及马赫数影响规律 期刊论文
推进技术, 2020, 卷号: 42, 期号: 10, 页码: 2207-2217
Authors:  贺理浩;  张启帆;  岳连捷;  张新宇;  王卫星;  谭慧俊
Adobe PDF(9600Kb)  |  Favorite  |  View/Download：271/41  |  Submit date：2021/11/12
高速进气道  低马赫数不起动  非定常  气动力  自起动  
Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
Authors:  Meng Y(孟宇);  Gu HB(顾洪斌);  Zhuang JH(庄金衡);  Sun WM(孙文明);  Gao ZB(高占彪);  Lian H(连欢);  Yue LJ(岳连捷);  Chang XY(张新宇)
View  |  Adobe PDF(3099Kb)  |  Favorite  |  View/Download：377/99  |  Submit date：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration  
真实气体效应对Ma10级进气道流动的影响 期刊论文
推进技术, 2019, 卷号: 40, 期号: 05, 页码: 1042-1050
Authors:  张启帆;  岳连捷;  贾轶楠;  张新宇;  李欣;  高雄
View  |  Adobe PDF(1675Kb)  |  Favorite  |  View/Download：257/50  |  Submit date：2019/09/12
真实气体效应  高马赫数进气道  化学非平衡气体模型  热完全气体模型  前缘钝化  再起动性能  
Flow characteristics of hypersonic inlets with different cowl-lip blunting methods 期刊论文
SCIENCE CHINA-Physics, Mechanics & Astronomy, 2014, 卷号: 57, 期号: 4, 页码: 741-752
Authors:  Lu HB(卢洪波);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Yue LJ(岳连捷)
View  |  Adobe PDF(1133Kb)  |  Favorite  |  View/Download：962/263  |  Submit date：2014/04/15
Hypersonic Inlet  Cowl-lip Bluntness  Flow Characteristics  Shock Pattern  Shock Interference  
Interaction of isentropic compression waves with a bow shock 期刊论文
AIAA JOURNAL, 2013, 卷号: 51, 期号: 10, 页码: 2474-2484
Authors:  Lu HB(卢洪波);  Yue LJ(岳连捷);  Xiao YB(肖雅彬);  Zhang XY(张新宇);  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(764Kb)  |  Favorite  |  View/Download：774/290  |  Submit date：2014/01/17
Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Chen LH(陈立红);  Zhang XY(张新宇);  Xiao YB(肖雅彬)
View  |  Adobe PDF(1674Kb)  |  Favorite  |  View/Download：469/124  |  Submit date：2014/02/24
超燃冲压发动机尾喷管流线追踪设计 期刊论文
推进技术, 2011, 卷号: 32, 期号: 1, 页码: 91-96
Authors:  卢鑫;  岳连捷;  肖雅彬;  张新宇
Adobe PDF(436Kb)  |  Favorite  |  View/Download：805/237  |  Submit date：2012/04/01
三维尾喷管设计  流线追踪  超燃冲压发动机