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State Key ... [8]
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姜宗林 [8]
李进平 [8]
汪球 [5]
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俞鸿儒 [3]
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On theory and methods for advanced detonation-driven hypervelocity shock tunnels
期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors:
Jiang ZL(姜宗林)
;
Li JP(李进平)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Yu HR(俞鸿儒)
Adobe PDF(1090Kb)
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Submit date:2020/11/30
hypervelocity
shock tunnel
detonation driver
flight condition
tailored condition
test facilities
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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Submit date:2023/03/17
Experimental investigation of liquid film cooling in hypersonic flow
期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 4, 页码: 10
Authors:
Yuan CK(苑朝凯)
;
Li JP(李进平)
;
Jiang ZL(姜宗林)
;
Yu HR(俞鸿儒)
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View/Download:454/132
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Submit date:2019/06/10
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)
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Submit date:2018/10/30
copper calorimeter
high enthalpy shock tunnel
heat transfer
hypersonic
高超声速溢流冷却实验研究
期刊论文
力学学报, 2018, 卷号: 50, 期号: 1, 页码: 1-8
Authors:
苑朝凯
;
李进平
;
陈宏
;
姜宗林
;
俞鸿儒
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Submit date:2018/10/24
高超声速热防护
主动冷却
溢流冷却
液膜
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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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)
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  |  
Adobe PDF(679Kb)
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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.
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View/Download:556/233
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Submit date:2016/03/21
Aerodynamic Heating
Hypersonic
Shock Tunnel
Stanton Number
Sharp Cone