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Knowledge Management System of Institue of Mechanics, CAS
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姜宗林 [4]
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Funding Organization:National Natural Science Foundation of China
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Mitigation of Shock-Induced Separation Using Square-Shaped Micro-Serrations-A Preliminary Study
期刊论文
AEROSPACE, 2024, 卷号: 11, 期号: 2, 页码: 16
Authors:
Yu FY(于方游)
;
Gao ZB(高占彪)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Chen H(陈昊)
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View/Download:12/0
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Submit date:2024/05/21
micro-serration
separation control
shock wave/boundary layer interaction
Magnetic and Pressure Effects on E-H Mode Transition Power and Electron Energy Distribution in Helical Antenna-Coupled RF Plasma
期刊论文
IEEE TRANSACTIONS ON PLASMA SCIENCE, 2021, 卷号: 49, 期号: 9, 页码: 2806-2816
Authors:
Wang CS(王传胜)
;
Liu, Xuhui
;
Geng, Jinyue
;
Li F(李飞)
;
Lin X(林鑫)
;
Yu XL(余西龙)
Adobe PDF(3369Kb)
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Submit date:2021/11/01
E-H mode transition
electron energy distribution function (EEDF)
helical antenna
magnetic
Numerical Study of Turbulent Convective Heat Transfer of Aviation Kerosene in Coiled Pipes
期刊论文
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2021, 卷号: 143, 期号: 6, 页码: 6
Authors:
Fan WH(范文慧)
;
Zhong FQ(仲峰泉)
Adobe PDF(1552Kb)
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Submit date:2021/06/15
coiled pipe
kerosene flow
convective heat transfer
numerical study
Fluid-structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil system
期刊论文
NONLINEAR DYNAMICS, 2021, 页码: 22
Authors:
Zhu, Hong
;
Sun, Qinglin
;
Liu, Xuefeng
;
Liu, Jinglei
;
Sun, Hao
;
Wu WN(邬婉楠)
;
Tan, Panlong
;
Chen, Zengqiang
Adobe PDF(4213Kb)
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Submit date:2021/08/03
Fluid-structure interaction
Parafoil system
Flexible deformation
Trailing edge deflection
Aerodynamic performance
Dynamic model
Criteria for hypersonic airbreathing propulsion and its experimental verification
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:
Jiang ZL(姜宗林)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Wang C(王春)
;
Luo ZT(罗长童)
Adobe PDF(1806Kb)
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
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
Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 31, 页码: 15683-15696
Authors:
Xue R(薛瑞)
;
Zheng X
;
Yue LJ(岳连捷)
;
Zhang SK
;
Weng C
Adobe PDF(3251Kb)
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Submit date:2020/07/06
Compressible boundary layer combustion
Skin-friction reduction
Shock train/flame interaction
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)
Adobe PDF(2227Kb)
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Submit date:2019/10/21
Aerodynamic force measurement
Dynamic system
Impact response
Cross-validation
System identification
Numerical study of a fully confined supersonic slot impinging jet from bleed system
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Chang XY(张新宇)
Adobe PDF(3918Kb)
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Submit date:2019/09/09
Fully confined supersonic jet
Inclined impingement
Heat transfer
Boundary layer bleed
Numerical simulation
External-Compression Supersonic Inlet Free from Violent Buzz
期刊论文
AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523
Authors:
Chen H
;
Tan H
;
Liu YZ
;
Zhang QF(张启帆)
Adobe PDF(4679Kb)
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Submit date:2019/09/09