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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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State Key ... [6]
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汪球 [6]
赵伟 [6]
李进平 [5]
Li JW [2]
Lu P [2]
姜宗林 [2]
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Indexed By:EI
Creator:汪球
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Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
Authors:
Luo K(罗凯)
;
Wang Q(汪球)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
Adobe PDF(2023Kb)
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View/Download:347/107
  |  
Submit date:2020/11/30
Quasi-one-dimensional
Detonation
Shock tunnel
Shock speed
Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
Authors:
Wang Q(汪球)
;
Luo K(罗凯)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
Adobe PDF(2057Kb)
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View/Download:276/85
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Submit date:2020/08/26
Shock tunnel
Detonation driver
Diaphragm
Dual ignition
High-enthalpy flow
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)
Adobe PDF(1085Kb)
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View/Download:441/103
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Submit date:2019/05/29
Heat transfer measurement
Lateral heat conduction
Shock tunnel
Thermocouple
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.
Adobe PDF(419Kb)
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View/Download:448/117
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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)
Adobe PDF(679Kb)
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View/Download:414/78
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Submit date:2018/01/16
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
Adobe PDF(468Kb)
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View/Download:318/86
  |  
Submit date:2018/01/16
Detonation
Gas Dynamics
Hypersonic Flow
Shock Tubes
Supersonic Aerodynamics