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Influence of test model material on the accuracy of transient heat transfer measurements in impulse facilities 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2019, 卷号: 104, 页码: 59-66
Authors:  Wang Q(汪球);  Olivier H;  Einhoff J;  Li JP(李进平);  Zhao W(赵伟)
Favorite  |  View/Download:61/0  |  Submit date:2019/05/29
Heat transfer measurement  Lateral heat conduction  Shock tunnel  Thermocouple  Hypersonic  
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;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
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copper calorimeter  high enthalpy shock tunnel  heat transfer  hypersonic  
高超声速绕平板直立舵干扰气动热研究 期刊论文
中北大学学报(自然科学版), 2017, 卷号: 38, 期号: 05, 页码: 609-613
Authors:  栗继伟;  汪球;  赵伟
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高超声速  激波/边界层干扰  气动热  激波风洞  
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.
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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)
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Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis  
Performance of a detonation driven shock tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Li JW;  Wang Q(汪球);  Zhao W(赵伟);  Lu P;  Tan YX
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Detonation  Gas Dynamics  Hypersonic Flow  Shock Tubes  Supersonic Aerodynamics  
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.
Adobe PDF(763Kb)  |  Favorite  |  View/Download:272/124  |  Submit date:2016/03/21
Aerodynamic Heating  Hypersonic  Shock Tunnel  Stanton Number  Sharp Cone  
高焓流动中电子密度的静电探针测试技术研究 期刊论文
中国科学. 技术科学, 2016, 卷号: 46, 期号: 5, 页码: 500-508
Authors:  汪球;  黄建栋;  聂春生;  赵伟;  余西龙
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High Enthalpy  Shock Tunnel  Electron Denstiy  Electrostatci Probe  
爆轰驱动膨胀管性能研究 期刊论文
航空学报, 2016, 卷号: 37, 期号: 3, 页码: 810-816
Authors:  周凯;  汪球;  胡宗民;  姜宗林
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Hypervelocity  Detonation-driven  Expansion Tube  Performance Study  Experimental Tests  Numerical Simulation  
高焓激波风洞有效试验时间的诊断 期刊论文
航空学报, 2015, 卷号: 36, 期号: 11, 页码: 3534-3539
Authors:  汪球;  赵伟;  余西龙;  姜宗林
Adobe PDF(354Kb)  |  Favorite  |  View/Download:149/26  |  Submit date:2016/08/22
高焓激波风洞  有效试验时间  爆轰驱动  静电探针  压力