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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 ... [5]
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姜宗林 [5]
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Indexed By:EI
Creator:姜宗林
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Date Issued:2017
Language:英语
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Numerical study of inflow equivalence ratio inhomogeneity on oblique detonation formation in hydrogen-air mixtures
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 256-263
Authors:
Fang YS(方宜申)
;
Hu ZM(胡宗民)
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Ng HD
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Adobe PDF(2663Kb)
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View/Download:399/102
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Submit date:2018/02/08
Oblique Detonation
Equivalence Ratio
Mixture Inhomogeneity
Detailed Chemistry
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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View/Download:379/95
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Submit date:2017/10/25
Shock Wave
Imperfect Gas
Heterogeneous
Theoretical Solution
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel
期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
Authors:
Liu YF(刘云峰)
;
Wang YP(汪运鹏)
;
Yuan CK(苑朝凯)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
;
Liu, YF (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:532/133
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Submit date:2017/08/22
Aerodynamic Force And Moment Measurement
10° Half-angle Cone Model
Jf12
Real-gas Effects
Shock Tunnel
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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View/Download:412/77
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Submit date:2018/01/16
Calibration
Detonation
Heat Transfer
Nozzles
Spacecraft
Supersonic Aerodynamics
Thermodynamics
Uncertainty Analysis