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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)
Favorite  |  View/Download:44/0  |  Submit date:2022/01/12
Airbreathing engine  Compression efficiency  Compression quality  Inlet  Self-consistency  
一种高焓超声速风洞气流生成方法 专利
发明专利. 一种高焓超声速风洞气流生成方法, 专利号: ZL202010322141.0, 申请日期: 2020-04-22, 授权日期: 2021-06-04
Inventors:  顾洪斌;  张新宇
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Heterostructured materials: superior properties from hetero-zone interaction 期刊论文
MATERIALS RESEARCH LETTERS, 2021, 卷号: 9, 期号: 1, 页码: 1-31
Authors:  Zhu YT;  Ameyama K;  Anderson PM;  Beyerlein IJ;  Gao HJ;  Kim HS;  Lavernia E;  Mathaudhu S;  Mughrabi H;  Ritchie RO;  Tsuji N;  Zhang XY;  Wu XL(武晓雷)
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Heterostructured materials  synergy  heterostructures  hetero-deformation induced (HDI) hardening  back stress  forward stress  
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
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Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
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)
Adobe PDF(3937Kb)  |  Favorite  |  View/Download:21/0  |  Submit date:2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
一种用于纯净空气风洞的密封膨胀节 专利
发明专利. 一种用于纯净空气风洞的密封膨胀节, 专利号: ZL201810506583.3,
Inventors:  孟东东;  张新宇;  林建民
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一种激光诱导荧光聚焦纹影系统 专利
发明专利. 一种激光诱导荧光聚焦纹影系统, 专利号: ZL201910435874.2,
Inventors:  连欢;  周芮旭;  张新宇
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Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
Authors:  Yang L;  Yue LJ(岳连捷);  Zhang QF(张启帆);  Zhang XY(张新宇)
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Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
Experimental and numerical investigation on flow and heat transfer of impingement jet cooling of kerosene 期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2020, 卷号: 116, 页码: 8
Authors:  Du MM(杜蒙蒙);  Zhong FQ(仲峰泉);  Xing YF(邢云绯);  Zhang XY(张新宇)
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Impingement jets  Kerosene  Heat transfer coefficient  Pressure loss  Reynolds number