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Knowledge Management System of Institue of Mechanics, CAS
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张新宇 [3]
岳连捷 [2]
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Indexed By:EI
Date Issued:2019
Funding Organization:National Natural Science Foundation of China
Document Type:期刊论文
Community:高温气体动力学国家重点实验室
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Magnetic Actuation of Flexible Microelectrode Arrays for Neural Activity Recordings
期刊论文
NANO LETTERS, 2019, 卷号: 19, 期号: 11, 页码: 8032-8039
Authors:
Gao L
;
Wang JF
;
Guan SL
;
Du MD
;
Wu K(吴坤)
;
Xu K
;
Zou L
;
Tian HH
;
Fang Y
Adobe PDF(7003Kb)
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Submit date:2020/03/11
flexible microelectrode
magnetic actuation
nanoscale roughness
neural recording
inflammatory response
Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
Authors:
Zhang X(张旭)
;
Yue LJ(岳连捷)
;
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
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View/Download:364/128
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Submit date:2020/03/21
Hysteresis
Dual-mode scramjet
Supersonic combustion
Mode transition
Flame stabilization
Combustion oscillation
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors:
Fan WH(范文慧)
;
Zhong FQ(仲峰泉)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
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Submit date:2020/03/11
Wall heat flux
Numerical simulation
Ethylene
Supersonic combustor
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)
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Submit date:2019/09/09
Fully confined supersonic jet
Inclined impingement
Heat transfer
Boundary layer bleed
Numerical simulation
Numerical simulation of the interaction of two shear layers in double backward-facing steps
期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 5, 页码: 15
Authors:
Deng F(邓放)
;
Han GL(韩桂来)
;
Liu MK(刘美宽)
;
Ding, J
;
Weng, PF
;
Jiang ZL(姜宗林)
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Submit date:2019/10/21
Numerical study of chemically reacting flow in a shock tube using a high-order point-implicit scheme
期刊论文
COMPUTERS & FLUIDS, 2019, 卷号: 184, 页码: 107-118
Authors:
Chen S
;
Sun QH(孙泉华)
;
Klioutchnikov I
;
Olivier H
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Submit date:2019/06/10
Shock wave/boundary-layer interactions
Real gas effects
Chemical nonequilibrium
High-order scheme
Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules
期刊论文
ACTA ASTRONAUTICA, 2019, 卷号: 157, 页码: 189-198
Authors:
Zhong K
;
Yan C
;
Chen SS
;
Wang XY(王小永)
;
Ju SJ
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View/Download:251/74
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Submit date:2019/05/29
Aeroheating
Heatshield configuration
Sphere-cone angle
Mars
Turbulent