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Numerical study on initiation of oblique detonations in hydrogen-air mixtures with various equivalence ratios 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 卷号: 49, 页码: 130-134
作者:  Zhang YN;  Gong JS;  Wang T(王涛);  Zhang, YN (reprint author), Beijing Power Machinery Res Inst, State Key Lab Laser Prop & Applicat, Beijing 100074, Peoples R China.
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Detonation  Hydrogen  Initiation  Hypersonic  
Comparative study on aerodynamic heating under perfect and nonequilibrium hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 2, 页码: 624701
作者:  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Aerodynamic Heating  Hypersonic  Shock Tunnel  Stanton Number  Sharp Cone  
Design of a pulse-type strain gauge balance for a long-test-duration hypersonic shock tunnel 期刊论文
SHOCK WAVES, 2016, 卷号: 26, 期号: 6, 页码: 835-844
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Wang, Y (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
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Hypersonic Shock Tunnel  Force Measurement  Strain Gauge Balance  
Numerical investigation on the thermal protection mechanism for blunt body with forward-facing cavity 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 7, 页码: 1120-1129
作者:  Li, XD;  Hu ZM(胡宗民);  Jiang ZL(姜宗林);  Hu, ZM (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Hypersonic Flow  Aerodynamic Heating  Thermal Protection System  Forward-facing Cavity  
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.
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  
Theoretical calculation of mid-infrared spectra from hypersonic non-ablative sphere 会议论文
International Symposium on Infrared Technology and Application / International Symposium on Robot Sensing and Advanced Control, Beijing, PEOPLES R CHINA, MAY 09-11, 2016
作者:  Wu J;  Yu XL(余西龙);  Zhu XJ;  Ma J;  Mao HX;  Wu, J (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Wu, J (reprint author), Sci & Technol Opt Radiat Lab, Beijing 100854, Peoples R China.
Adobe PDF(1160Kb)  |  收藏  |  浏览/下载:272/82  |  提交时间:2017/05/12
Hypersonic  Mid-infrared  Atom  Diatomic Molecule  Partition-functions  Molecules  Air  
基于实验设计方法的高超声速飞机前缘型线优化分析 期刊论文
力学学报, 2016, 卷号: 48, 期号: 2, 页码: 290-299
作者:  胡守超;  崔凯;  李广利;  肖尧;  司徒明
Adobe PDF(1239Kb)  |  收藏  |  浏览/下载:335/61  |  提交时间:2016/12/16
Hypersonic Airplane  Air-breathing Vehicle  Shape Optimization  Parameterization  Uniform Design