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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：329/81  |  提交时间：2016/09/14
Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
Development of efficient and accurate skeletal mechanisms for hydrocarbon fuels and kerosene surrogate 期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 5, 页码: 732-740
作者:  Zhong FQ(仲峰泉);  Ma SG;  Zhang XY(张新宇);  Sung CJ;  Niemeyer KE;  Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1318Kb)  |  收藏  |  浏览/下载：288/91  |  提交时间：2016/01/08
Reduced Chemistry  Hydrocarbons  Directed Relation Graph  Ignition Delay Time  
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：447/125  |  提交时间：2015/10/21
Arc-heated Supersonic Jet  Low-power  Real Flow  Viscosity Effect  Low Reynolds Number  
Measurements of non-equilibrium and equilibrium temperature behind a strong shock wave in simulated martian atmosphere 期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 5, 页码: 1296-1302
作者:  Lin X;  Yu XL(余西龙);  Li F(李飞);  Zhang SH(张少华);  Xin JG;  Zhang XY(张新宇);  Yu, XL;  Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(828Kb)  |  收藏  |  浏览/下载：799/241  |  提交时间：2013/01/18
Radiation Measurements  Shock Wave  Mars Re-entry  Rotational Temperature  Vibrational Temperature  Radiation Measurements  Cn  Entry  Tube  Mixtures  Model