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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... [26]
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姜宗林 [26]
赵伟 [26]
汪球 [14]
王春 [7]
李进平 [6]
滕宏辉 [5]
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11532014) [1]
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Creator:姜宗林
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Creator:赵伟
Community:高温气体动力学国家重点实验室
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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)
Adobe PDF(240Kb)
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Submit date:2023/03/17
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)
Adobe PDF(299Kb)
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Submit date:2023/03/17
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)
Adobe PDF(1208Kb)
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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.
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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:421/79
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Submit date:2018/01/16
Calibration
Detonation
Heat Transfer
Nozzles
Spacecraft
Supersonic Aerodynamics
Thermodynamics
Uncertainty Analysis
高频多脉冲爆轰起爆点火器
专利
发明专利. 高频多脉冲爆轰起爆点火器, 专利号: ZL201310031205.1, 申请日期: 2013-01-28, 授权日期: 2016-03-23
Inventors:
姜宗林
;
王春
;
赵伟
Adobe PDF(251Kb)
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Submit date:2016/03/30
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)
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Submit date:2016/03/21
Aerodynamic Heating
Hypersonic
Shock Tunnel
Stanton Number
Sharp Cone
长试验时间激波风洞测力技术研究
期刊论文
力学学报, 2016, 卷号: 48, 期号: 3, 页码: 545-556
Authors:
汪运鹏
;
刘云峰
;
苑朝凯
;
罗长童
;
王春
;
胡宗民
;
韩桂来
;
赵伟
;
姜宗林
Adobe PDF(8800Kb)
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Submit date:2016/12/16
Shock Tunnel
Long-test Duration
Force Measurement
Strain-gaged Balance
长试验时间激波风洞测力技术研究
会议论文
中国力学大会-2015, 中国上海, 2015-08-16
Authors:
汪运鹏
;
刘云峰
;
姜宗林
;
赵伟
;
苑朝凯
;
罗长童
;
王春
;
胡宗民
Adobe PDF(430Kb)
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Submit date:2016/08/16
测力
激波风洞
动态校准
试验需求
试验时间
尖锥
刚度特性
单元结构
优化设计
最大载荷
高焓激波风洞喷管流场非平衡特性研究
期刊论文
空气动力学学报, 2015, 卷号: 33, 期号: 1, 页码: 66-71
Authors:
汪球
;
赵伟
;
滕宏辉
;
姜宗林
Adobe PDF(1866Kb)
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Submit date:2015/11/02
爆轰驱动
非平衡
焓值
激波风洞