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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 [34]
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Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel
期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(2434Kb)
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Submit date:2022/08/23
Aerodynamic Coefficients
Two Stage to Orbit
Aerodynamic Performance
Hypersonic Flight
Hypersonic Wind Tunnels
Solenoid Valves
Oblique Shock
Pneumatic Actuator
Hypersonic Flows
Computer Aided Engineering
Analytic investigation on error of heat flux measurement and data processing for large curvature models in hypersonic shock tunnels
期刊论文
APPLIED MATHEMATICS LETTERS, 2022, 卷号: 134, 页码: 8
Authors:
Han GL(韩桂来)
;
Qi L(齐力)
;
Jiang ZL(姜宗林)
Adobe PDF(1715Kb)
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Submit date:2022/11/08
Heat flux
Measurement
Data processing
Error
Approximate solution
A theoretical method for solving shock relations coupled with chemical equilibrium and its applications
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 6, 页码: 47-62
Authors:
Zhang, Zijian
;
Wen, Chihyung
;
Zhang WS(张文硕)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(3178Kb)
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Submit date:2022/07/18
Chemical equilibrium
Detonation
Dissociated air
Shock relation
Theoretical solution
Reconstructing shock front of unstable detonations based on multi-layer perceptron
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
Authors:
Zhou, Lin
;
Teng, Honghui
;
Ng, Hoi Dick
;
Yang PF(杨鹏飞)
;
Jiang ZL(姜宗林)
Adobe PDF(6382Kb)
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Submit date:2021/11/01
Cellular detonation
Lead shock evolution
Multi-layer perceptron
Numerical simulations
Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiation in a high enthalpy hypersonic tunnel
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 7
Authors:
Peng, Di
;
Liu, Xu
;
Jiao, Lingrui
;
Li, Ziyan
;
Wen, Xin
;
Yuan CK(苑朝凯)
;
Han GL(韩桂来)
;
Liu YF(刘云峰)
;
Liu, Yingzheng
;
Jiang ZL(姜宗林)
Adobe PDF(3477Kb)
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Submit date:2021/03/30
Temperature-sensitive paint
Time-resolved measurement
Hypersonic flow
Background radiation
Formation of stabilized oblique detonation waves in a combustor
期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors:
Zhang ZJ(张子健)
;
Wen, Chihyung
;
Zhang WS(张文硕)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(3599Kb)
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Submit date:2021/03/03
Oblique detonation wave
Combustor
Oblique detonation engine
Normal detonation wave
Boundary layer separation
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)
Adobe PDF(2818Kb)
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Submit date:2021/01/29
Shock-shock interaction
Machine learning
Hypersonic flow
Impinging jet
Genetic programming
Triple point
Intelligent Force-Measurement System Use in Shock Tunnel
期刊论文
SENSORS, 2020, 卷号: 20, 期号: 21, 页码: 6179
Authors:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(2149Kb)
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Submit date:2020/12/28
artificial intelligence
BALANCE SYSTEM
deep learning
DESIGN
dynamic calibration
FLOWS
force-measurement system
strain-gauge balance
Impulse force-measurement system
期刊论文
SHOCK WAVES, 2020, 页码: 11
Authors:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(1551Kb)
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Submit date:2020/11/30
Shock tunnel
High enthalpy
Aerodynamic force measurement
Strain gauge balance