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Influence of Dual Ignition on Test Conditions of a High-Enthalpy Shock Tunnel 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:  Wang Q(汪球);  Zhao W(赵伟);  Li JW(栗继伟);  Li JP(李进平);  Lu P(卢盼);  Jiang ZL(姜宗林)
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Comparative Heat Flux Measurement of a Sharp Cone Between Three Hypersonic Test Facilities at LHD 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:  Wang Q(汪球);  Lu P(卢盼);  Li JW(栗继伟);  Wu S(吴松);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
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Performance of Copper Calorimeter for Heat Transfer Measurement in High Enthalpy Shock Tunnel 期刊论文
JOURNAL OF THERMAL SCIENCE, 2018, 卷号: 27, 期号: 4, 页码: 373-381
Authors:  Wang Q(汪球);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1208Kb)  |  Favorite  |  View/Download:657/135  |  Submit date:2018/10/30
copper calorimeter  high enthalpy shock tunnel  heat transfer  hypersonic  
Influence of Thermal Sensor Installation on Measuring Accuracy at Stagnation Points 期刊论文
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2017, 卷号: 31, 期号: 2, 页码: 318-323
Authors:  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, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
View  |  Adobe PDF(419Kb)  |  Favorite  |  View/Download:437/116  |  Submit date:2017/10/27
Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Wang Q(汪球);  Li JW;  Lu P;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
View  |  Adobe PDF(679Kb)  |  Favorite  |  View/Download:401/74  |  Submit date:2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis  
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
Authors:  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.
View  |  Adobe PDF(763Kb)  |  Favorite  |  View/Download:543/230  |  Submit date:2016/03/21
Aerodynamic Heating  Hypersonic  Shock Tunnel  Stanton Number  Sharp Cone  
高超声速电离绕流中电子密度的静电探针测量方法研究 期刊论文
实验流体力学, 2013, 卷号: 27, 期号: 6, 页码: 64-69+85
Authors:  汪球;  赵伟;  余西龙;  姜宗林
Adobe PDF(487Kb)  |  Favorite  |  View/Download:901/236  |  Submit date:2014/01/24
静电探针  电子密度  高超声速  高焓激波风洞  Electrostatic Probe  Electron Density  Hypersonic  High Enthalpy Shock Tunnel  
The criterion of the existence or inexistence of transverse shock wave at wedge supported oblique detonation wave 期刊论文
Acta Mechanica Sinica, 2011, 卷号: 27, 期号: 5, 页码: 611-619
Authors:  Wang AF(王爱峰);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Wang, AF (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China
Adobe PDF(1008Kb)  |  Favorite  |  View/Download:999/222  |  Submit date:2012/04/01
Oblique Detonation Wave  Transverse Shock Wave  Oblique Shock Wave  Transition  Numerical Simulations  Numerical-simulation