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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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姜宗林 [10]
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Creator:姜宗林
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Document Type:期刊论文
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Advances in critical technologies for hypersonic and high-enthalpy wind tunnel
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:
Jiang ZL(姜宗林)
;
Hu ZM(胡宗民)
;
Wang YP(汪运鹏)
;
Han GL(韩桂来)
Adobe PDF(1129Kb)
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Submit date:2021/03/30
High-enthalpy flow
Hypersonic wind tunnel
Aerospace vehicle
Aerodynamic balance
Heat flux sensor
Optical measurement technique
Parameter-correlation study on shock-shock interaction using a machine learning method
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247
Authors:
Peng J(彭俊)
;
Luo ZT(罗长童)
;
Han ZJ(韩子健)
;
Hu ZM(胡宗民)
;
Han GL(韩桂来)
;
Jiang ZL(姜宗林)
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Submit date:2021/01/29
Shock-shock interaction
Machine learning
Hypersonic flow
Impinging jet
Genetic programming
Triple point
Weighting by Cross-Validation: A Calibration Method for Force Measurements via Transient Response Analysis
期刊论文
EXPERIMENTAL TECHNIQUES, 2019, 卷号: 43, 期号: 4, 页码: 469-478
Authors:
Luo ZT(罗长童)
;
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Li JP(李进平)
;
Jiang ZL(姜宗林)
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Submit date:2019/10/21
Aerodynamic force measurement
Dynamic system
Impact response
Cross-validation
System identification
Continuum perspective of bulk viscosity in compressible fluids
期刊论文
JOURNAL OF FLUID MECHANICS, 2017, 卷号: 812, 页码: 966-990
Authors:
Li XD
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
;
Hu, ZM (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:450/150
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Submit date:2017/04/26
Starting Process in a Large-Scale Shock Tunnel
期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
Authors:
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
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View/Download:350/98
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Submit date:2017/09/19
Theoretical solutions to three-dimensional asymmetrical shock/shock interaction
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 8, 页码: 1208-1216
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Hu ZM(胡宗民)
;
Li XD
;
Jiang ZL(姜宗林)
;
Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
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View/Download:501/122
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Submit date:2016/12/08
3d Asymmetrical Shock/shock Interaction
Spatial-dimension Reduction
Mach Reflection
Flow Field
Theoretical Analysis
Adaptive space transformation: An invariant based method for predicting aerodynamic coefficients of hypersonic vehicles
期刊论文
Engineering Applications of Artificial Intelligence, 2015, 卷号: 46, 页码: 93-103
Authors:
Luo CT(罗长童)
;
Hu ZM(胡宗民)
;
Zhang SL
;
Jiang ZL(姜宗林)
;
Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2016/01/07
Aerodynamic Coefficient
Data Correlation
Scaling Parameter
Genetic Programming
Invariant
Numerical analysis of spatial evolution of the small signal gain in a chemical oxygen-iodine laser operating without primary buffer gas
期刊论文
Optics and Laser Technology, 2008, 卷号: 40, 期号: 1, 页码: 13-20
Authors:
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
;
Myong R
;
Cho T
;
Myong, R (reprint author), Gyeongsang Natl Univ, Res Ctr Aircraft Parts Technol, Jinju 660701, South Korea.
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View/Download:844/182
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Submit date:2009/08/03
Chemical Oxygen-iodine Laser (Coil)
Without Buffer Gas
Interleaved Jet
Slit-nozzle
Temperature
Injection
Schemes
Numerical Study on the Performance of Nozzle Flow for Supersonic Chemical Oxygen-Iodine Lasers
期刊论文
ACTA MECHANICA SINICA, 2008, 卷号: 24, 期号: 2, 页码: 133-142
Authors:
Hu ZM(胡宗民)
;
Lv JM(吕俊明)
;
Jiang ZL(姜宗林)
;
Myong RS
;
Cho TH
;
Jiang, ZL (reprint author), CAS, Inst Mech, LHD, Beijing 100080, Peoples R China.
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Submit date:2016/01/11
Chemical Oxygen-iodine Laser (Coil)
Numerical Simulation
Small Signal Gains
Unsteady Structures
NUMERICAL ANALYSIS OF THE FLOWFIELD IN A SUPERSONIC COIL WITH AN INTERLEAVED JET CONFIGURATION AND ITS EFFECT ON THE GAIN DISTRIBUTION
期刊论文
Engineering Applications of Computational Fluid Mechanics, 2007, 卷号: 1, 期号: 3, 页码: 207-215
Authors:
Hu ZM(胡宗民)
;
Myong RS
;
Nguyen AT
;
Singh VP
;
Jiang ZL(姜宗林)
;
Cho TH
;
Myong, RS (reprint author), Gyeongsang Natl Univ, Res Ctr Aircraft Parts Technol, Jinju 660701, South Korea.
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Submit date:2009/08/03
Coil Without Buffer
Interleaved Jet
Flowfield
Small Signal Gain