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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
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  
Study of coupled effect of impingement jet cooling of kerosene with solid structure 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2019, 卷号: 62, 期号: 11, 页码: 2021-2028
作者:  Du MM(杜蒙蒙);  Zhong FQ(仲峰泉);  Xing YF(邢云绯);  Zhang XY(张新宇)
浏览  |  Adobe PDF(2806Kb)  |  收藏  |  浏览/下载：348/84  |  提交时间：2020/03/21
impingement jet cooling  hydrocarbon fuel  heat transfer enhancement  fluid-solid coupling  
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
作者:  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.
浏览  |  Adobe PDF(1162Kb)  |  收藏  |  浏览/下载：327/81  |  提交时间：2016/09/14
Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor 期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
作者:  Wang X;  Zhong FQ(仲峰泉);  Gu HB(顾宏斌);  Zhang XY(张新宇);  Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(4711Kb)  |  收藏  |  浏览/下载：295/128  |  提交时间：2016/01/08
Supersonic Combustor  Convective Heat Transfer  Numerical Study  Wall Heat Flux  
Numerical study of heat transfer deterioration of turbulent supercritical kerosene flow in heated circular tube 期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2015, 卷号: 85, 页码: 1003-1011
作者:  Dang GX;  Zhong FQ(仲峰泉);  Zhang YJ;  Zhang XY(张新宇);  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Bei Si Huan Xi Rd 15, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(2856Kb)  |  收藏  |  浏览/下载：458/133  |  提交时间：2015/06/12
Supercritical Kerosene  Convective Heat Transfer  Turbulent Flow  Numerical Study  
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
作者:  Wang ZP(王知溥);  Li F(李飞);  Gu HS;  Yu XL(余西龙);  Zhang XY(张新宇);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1112Kb)  |  收藏  |  浏览/下载：536/225  |  提交时间：2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas  
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
作者:  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.
浏览  |  Adobe PDF(860Kb)  |  收藏  |  浏览/下载：437/187  |  提交时间：2015/04/28
Hypersonic Scramjet Test Tunnel  Nozzle  Aerodynamic Heating  Convective Heat Transfer  
Quasi-One-Dimensional Multimodes Analysis for Dual-Mode Scramjet 期刊论文
JOURNAL OF PROPULSION AND POWER, 2014, 卷号: 30, 期号: 6, 页码: 1559-1567
作者:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Li F(李飞);  Zhang XY(张新宇);  Tian, L (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(7587Kb)  |  收藏  |  浏览/下载：585/135  |  提交时间：2014/12/18
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
作者:  Lu HB(卢洪波);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Yue LJ(岳连捷)
浏览  |  Adobe PDF(1133Kb)  |  收藏  |  浏览/下载：905/257  |  提交时间：2014/04/15
Hypersonic Inlet  Cowl-lip Bluntness  Flow Characteristics  Shock Pattern  Shock Interference  
Theoretical analysis of effects of boundary layer bleed on scramjet thrust 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 10, 页码: 1952-1961
作者:  Yue LJ(岳连捷);  Xu XK(徐显坤);  Zhang XY(张新宇);  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(788Kb)  |  收藏  |  浏览/下载：877/258  |  提交时间：2013/10/23
Scramjet  Boundary Layer Bleed  Theoretical Analysis  Engine Thrust