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韩桂来 [9]
姜宗林 [7]
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Numerical studies of flow patterns and fuel distribution of tandem-arranged multi jets in a hypersonic crossflow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 139, 页码: 108383
Authors:
Wang JL(王嘉麟)
;
Han GL(韩桂来)
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Submit date:2023/07/17
Hypersonic flow
Tandem -arranged jets
Streamline pattern
Vortex structure
Fuel -air mixing
Theoretical, numerical and experimental study of hypersonic boundary layer transition: Blunt circular cone
期刊论文
APPLIED THERMAL ENGINEERING, 2021, 卷号: 194, 页码: 14
Authors:
Chen, Jianqiang
;
Yi, Shihe
;
Li XL(李新亮)
;
Han GL(韩桂来)
;
Zhang, Yifeng
;
Yang, Qiang
;
Yuan, Xianxu
Adobe PDF(11175Kb)
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Submit date:2021/08/03
Hypersonic boundary layer
Stability
Transition
Thermal protection
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)
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Submit date:2021/03/30
Temperature-sensitive paint
Time-resolved measurement
Hypersonic flow
Background radiation
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
Numerical investigation of the axial impulse load during the startup in the shock tunnel
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342
Authors:
Meng BQ(孟宝清)
;
Han GL(韩桂来)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
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View/Download:271/88
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Submit date:2018/10/30
Hypersonic
Shock tunnel
Start-up process
Impulse force
Vibration
Aerodynamic measurement of a large aircraft model in hypersonic flow
期刊论文
CHINESE PHYSICS B, 2017, 卷号: 26, 期号: 11, 页码: 114702-1-114702-6
Authors:
Meng BQ(孟宝清)
;
Han GL(韩桂来)
;
Zhang DL(张德良)
;
Jiang ZL(姜宗林)
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Submit date:2017/12/18
Hypersonic
Aerodynamic Measurement
Theoretical Study
Vibration
Approximate analytic solution of heat conduction in hollow semi-spheres flying at hypersonic speed
期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2013, 卷号: 43, 页码: 46-52
Authors:
Han GL(韩桂来)
;
Jiang ZL(姜宗林)
;
Han, GL (reprint author), Chinese Acad Sci, Stake Key Lab High Temp Gas Dynam LHD, Inst Mech, Beijing 100190, Peoples R China.
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View/Download:1115/333
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Submit date:2013/05/31
Heat Conduction
Theoretical Investigation
Approximate Solution
Hypersonic
Experimental Demonstration Of A New Concept Of Drag Reduction And Thermal Protection For Hypersonic Vehicles
期刊论文
Acta Mechanica Sinica, 2009, 卷号: 25, 期号: 3, 页码: 417-419
Authors:
Jiang ZL(姜宗林)
;
Liu YF(刘云峰)
;
Han GL(韩桂来)
;
Zhao W(赵威)
;
Jiang ZL
Adobe PDF(226Kb)
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View/Download:908/217
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Submit date:2009/08/03
Hypersonic Vehicle
Shock-reconstruction
Drag Reduction
Thermal Protection
Spike And Lateral Jets