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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
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高速进气道  低马赫数不起动  非定常  气动力  自起动  
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH(马生虎);  Zhang QF(张启帆);  Zhang, Peng;  Zhang XY(张新宇)
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Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors:  Fan WH(范文慧);  Zhong FQ(仲峰泉);  Ma SG(马素刚);  Zhang XY(张新宇)
View  |  Adobe PDF(4075Kb)  |  Favorite  |  View/Download：312/92  |  Submit date：2020/03/11
Wall heat flux  Numerical simulation  Ethylene  Supersonic combustor  
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：240/48  |  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  
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
H_2O/CO_2污染对RP-3航空煤油着火特性的影响 期刊论文
推进技术, 2015, 卷号: 36, 期号: 3, 页码: 336-344
Authors:  梁金虎;  王苏;  张灿;  张胜涛;  岳连捷;  范秉诚;  张新宇;  崔季平
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污染效应  着火延时  煤油  H2o  Co2  激波管  
Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475
Authors:  Xing YF(邢云绯);  Zhong FQ(仲峰泉);  Li DX(李东霞);  Zhang XY(张新宇);  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(860Kb)  |  Favorite  |  View/Download：457/198  |  Submit date：2015/04/28
Hypersonic Scramjet Test Tunnel  Nozzle  Aerodynamic Heating  Convective Heat Transfer  
高超声速进气道快速破膜开启的流动特性 期刊论文
航空学报, 2015, 卷号: 36, 期号: 6, 页码: 1795-1804
Authors:  徐骁;  岳连捷;  卢洪波;  肖雅彬;  张新宇
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高超声速进气道  破膜开启  非定常效应  激波边界层相互作用  分离流  
The vitiation effects of water vapor and carbon dioxide on the autoignition characteristics of kerosene 期刊论文
Acta Mechanica Sinica, 2014, 卷号: 30, 期号: 4, 页码: 485-494
Authors:  Liang JH(梁金虎);  Wang S(王苏);  Zhang ST(张胜涛);  Yue LJ(岳连捷);  Fan BC(范秉诚);  Zhang XY(张新宇);  Cui JP(崔季平);  Wang S(王苏)
Adobe PDF(1351Kb)  |  Favorite  |  View/Download：893/221  |  Submit date：2014/08/14
Ignition Delay  Vitiation Effect  Kerosene  Water  Carbon Dioxide  Shock Tube