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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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李进平 [7]
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On the response of coaxial surface thermocouples for transient aerodynamic heating measurements
期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2017, 卷号: 86, 页码: 141-148
Authors:
Li JP(李进平)
;
Chen H(陈宏)
;
Zhang SZ(张仕忠)
;
Zhang XY(张晓源)
;
Yu HR(俞鸿儒)
;
Chen, H (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:430/92
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Submit date:2017/07/24
Heat Flux Measurement
Thermocouple
Response Characteristics
Shock Tube
飞剪帆船、竞速帆船和波形线理论
期刊论文
物理, 2017, 卷号: 46, 期号: 07, 页码: 460-461
Authors:
李进平
;
刘云峰
;
Larrie D.Ferreiro
;
Alexander Pollara
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View/Download:222/70
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Submit date:2017/12/22
弗劳德
航行速度
飞剪
物理规律
竞速
英国工程师
相似律
兴波阻力
工程师们
斯科特
Shock relations in gases of heterogeneous thermodynamic properties
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
Authors:
Hu ZM(胡宗民)
;
Zhou K(周凯)
;
Peng J(彭俊)
;
Li JP(李进平)
;
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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Submit date:2017/10/25
Shock Wave
Imperfect Gas
Heterogeneous
Theoretical Solution
α-Pu和δ-Pu电子结构的密度泛函理论计算
期刊论文
原子能科学技术, 2017, 卷号: 51, 期号: 04, 页码: 584-590
Authors:
朱芫江
;
高云亮
;
李进平
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View/Download:261/51
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Submit date:2017/12/22
Α-pu
Δ-pu
密度泛函理论
电子结构
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
Al辐照损伤初期的第一性原理研究
期刊论文
物理学报/ACTA PHYSICA SINICA, 2017, 卷号: 66, 期号: 5, 页码: 057104
Authors:
高云亮
;
朱芫江
;
李进平
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Submit date:2017/07/24
Al
辐照损伤
Irradiation Damage
点缺陷
Point Defect
第一性原理
First-principles
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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Submit date:2018/01/16
Calibration
Detonation
Heat Transfer
Nozzles
Spacecraft
Supersonic Aerodynamics
Thermodynamics
Uncertainty Analysis