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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.
Adobe PDF(4711Kb)  |  收藏  |  浏览/下载:298/130  |  提交时间:2016/01/08
Supersonic Combustor  Convective Heat Transfer  Numerical Study  Wall Heat Flux  
Wave system fitting: A new method for force measurements in shock tunnels with long test duration 期刊论文
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2015, 卷号: 62-63, 页码: 2841-2848
作者:  Luo CT(罗长童);  Wang YP(汪云鹏);  Wang C(王春);  Jiang ZL(姜宗林);  Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1074Kb)  |  收藏  |  浏览/下载:344/95  |  提交时间:2016/01/07
Aerodynamic Force Measurements  Strain Gauge Balance  Inertia Compensation  Signal Decomposition  Accelerometer-free  Shock Tunnels  
Tunable diode laser absorption spectroscopy measurements of high-pressure ammonium dinitramide combustion 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 45, 页码: 140-149
作者:  Yao, Zhaopu;  Zhang, Wei;  Wang, Meng;  Chen, Jun;  Shen, Yan;  Wei, Yanming;  Yu XL(余西龙);  Li F(李飞);  Ceng H(曾徽);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Unknown(1847Kb)  |  收藏  |  浏览/下载:239/69  |  提交时间:2015/10/21
Numerical study of oblique detonation wave initiation in a stoichiometric hydrogen-air mixture 期刊论文
PHYSICS OF FLUIDS, 2015, 卷号: 27, 期号: 9, 页码: 96101
作者:  Wang T;  Zhang YN;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Ng HD;  Wang, T (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Mechanisms for non-ideal flow in low-power arc-heated supersonic nozzles 期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 4, 页码: 500-511
作者:  Wu CK(吴承康);  Pan WX(潘文霞);  Meng X(孟显);  Wang, Hai-Xing;  Wu, CK (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(878Kb)  |  收藏  |  浏览/下载:450/126  |  提交时间:2015/10/21
Arc-heated Supersonic Jet  Low-power  Real Flow  Viscosity Effect  Low Reynolds Number  
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.
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Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas  
Study and prediction for the fire resistance of acid corroded intumescent coating 会议论文
9th International Symposium on Safety Science and Technology (ISSST), Beijing, PEOPLES R CHINA, NOV 04-06, 2014
作者:  Wang J;  Song WH;  Zhang M;  Chen Z(陈阵);  Song, WH (reprint author), Tianjin Polytech Univ, Environm & Chem Coll, Tianjin 300387, Peoples R China.
浏览  |  Adobe PDF(887Kb)  |  收藏  |  浏览/下载:349/63  |  提交时间:2016/06/28