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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
作者:  Dai, Chunliang;  Sun, Bo;  Yue LJ(岳连捷);  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yu, Jianyi
Adobe PDF(5674Kb)  |  收藏  |  浏览/下载：22/0  |  提交时间：2024/02/19
Scramjet inlet  Starting ability  Thermochemical  Work performance  
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
作者:  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)  |  收藏  |  浏览/下载：211/66  |  提交时间：2022/11/14
scramjet inlet  Lagrange optimization method  shock configuration  
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
作者:  Zhai J;  Zhang CA(张陈安);  Wang FM(王发民);  Zhang WW(张伟为)
Adobe PDF(4533Kb)  |  收藏  |  浏览/下载：144/35  |  提交时间：2022/12/20
Shock-wave/boundary-layer interaction  Backward-facing step  Flow separation  Hypersonic inlet  
Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet 期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 193, 页码: 237-254
作者:  Dai, Chunliang;  Sun, Bo;  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yue LJ(岳连捷)
Adobe PDF(13791Kb)  |  收藏  |  浏览/下载：156/35  |  提交时间：2022/05/17
Mach 12 scramjet inlet  High temperature  Non-equilibrium effects  Thermochemical  Inlet performance  
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
作者:  Chen KT(陈科挺);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(511Kb)  |  收藏  |  浏览/下载：194/36  |  提交时间：2022/01/12
Airbreathing engine  Compression efficiency  Compression quality  Inlet  Self-consistency  
Alleviation of lateral spillage of two-dimensional hypersonic inlet using waverider-configuration chines 期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS B, 2020, 卷号: 34, 期号: 14-16, 页码: 5
作者:  Zhai J;  Zhang CA(张陈安);  Wang FM(王发民);  Zhang WW
Adobe PDF(510Kb)  |  收藏  |  浏览/下载：176/70  |  提交时间：2020/08/26
Hypersonic inlet  lateral spillage  waverider design method  streamline tracing technology  mass-flow ratio  
Instability analysis for a centrifugal pump with straight inlet pipe using partially averaged Navier-Stokes model 期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2020, 页码: 16
作者:  Ye WX;  Qian ZD;  Huang RF(黄仁芳);  Li XJ;  Zhu ZC;  Luo XW
Adobe PDF(2510Kb)  |  收藏  |  浏览/下载：209/96  |  提交时间：2020/08/26
Centrifugal pump  inlet pipe  positive slope phenomenon  PANS model  
Effects of water vapor and temperature on NOx and CO emissions during converter gas combustion 期刊论文
FUEL, 2019, 卷号: 256, 页码: 6
作者:  Zhai YH(翟英华);  Li S(李森);  Yan, WP;  Wei XL(魏小林);  Zhang, LY;  Wang, YT
浏览  |  Adobe PDF(1712Kb)  |  收藏  |  浏览/下载：298/89  |  提交时间：2019/10/21
Water vapor concentration  Converter gas  Inlet temperature  CO emission  NO emission  
Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
作者:  Yue LJ(岳连捷);  Jia YN(贾轶南);  Xu X;  Zhang XY(张新宇);  Zhang P(张鹏)
浏览  |  Adobe PDF(2110Kb)  |  收藏  |  浏览/下载：366/135  |  提交时间：2018/10/30
Inlet restart  Cowl shock  Shock wave boundary layer interactions  
Design methodology for shape transition inlets based on constant contraction of discrete streamtubes 期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 230, 期号: 8, 页码: 1496-1506
作者:  Xiao YB(肖雅斌);  Yue LJ(岳连捷);  Ma SH;  Zhang XY(张新宇);  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100864, Peoples R China.
浏览  |  Adobe PDF(1353Kb)  |  收藏  |  浏览/下载：394/89  |  提交时间：2016/09/14
Hypersonic Inlet  Shape Transition  Inward Turning  Scramjet  Design Method