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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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Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Ma SH(马生虎)
;
Zhang QF(张启帆)
;
Zhang, Peng
;
Zhang XY(张新宇)
Adobe PDF(3937Kb)
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View/Download:216/56
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Submit date:2021/03/30
Adverse pressure gradient
Back pressure
Hysteresis effects
Non-uniform flow
Shock train
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)
Adobe PDF(4075Kb)
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View/Download:314/93
  |  
Submit date:2020/03/11
Wall heat flux
Numerical simulation
Ethylene
Supersonic combustor
Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
Authors:
Yue LJ(岳连捷)
;
Jia YN(贾轶南)
;
Xu X
;
Zhang XY(张新宇)
;
Zhang P(张鹏)
Adobe PDF(2110Kb)
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View/Download:387/138
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Submit date:2018/10/30
Inlet restart
Cowl shock
Shock wave boundary layer interactions
Downstream pressure variation induced hysteresis in the scramjet isolator
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Ma SH
;
Jia YN(贾轶南)
;
Zhang XY(张新宇)
;
Yue, Lianjie(yuelj@imech.ac.cn)
Adobe PDF(704Kb)
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View/Download:280/94
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Submit date:2018/01/16
Spacecraft
The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Jia YN(贾轶南)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Jia, Yinan(yuelj@imech.ac.cn)
Adobe PDF(566Kb)
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Submit date:2018/01/16
Boundary Layer Flow
Boundary Layers
Spacecraft
Wind Tunnels
Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor
期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
Authors:
Wang X
;
Zhong FQ(仲峰泉)
;
Gu HB(顾宏斌)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
Adobe PDF(4711Kb)
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Submit date:2016/01/08
Supersonic Combustor
Convective Heat Transfer
Numerical Study
Wall Heat Flux
Quasi-One-Dimensional Multimodes Analysis for Dual-Mode Scramjet
期刊论文
JOURNAL OF PROPULSION AND POWER, 2014, 卷号: 30, 期号: 6, 页码: 1559-1567
Authors:
Tian L
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Li F(李飞)
;
Zhang XY(张新宇)
;
Tian, L (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(7587Kb)
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Submit date:2014/12/18
Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition
会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:
Xiao YB(肖雅彬)
;
Yue LJ(岳连捷)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Xiao YB(肖雅彬)
Adobe PDF(1674Kb)
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View/Download:462/122
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Submit date:2014/02/24
Numerical study of ignition and combustion of partially cracked kerosene in a mach 2.5 supersonic model combustor
会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:
Zhong FQ(仲峰泉)
;
Chen LH(陈立红)
;
Chang XY(张新宇)
;
Zhong FQ(仲峰泉)
Adobe PDF(6469Kb)
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Submit date:2014/02/24
Simultaneous measurements of multiple flow parameters for scramjet characterization using tunable diode-laser sensors
期刊论文
Applied Optics, 2011, 卷号: 50, 期号: 36, 页码: 6697-6707
Authors:
Li F(李飞)
;
Yu XL(余西龙)
;
Gu HB(顾洪斌)
;
Li Z(李智)
;
Zhao Y
;
Ma L
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
Adobe PDF(1090Kb)
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View/Download:1211/258
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Submit date:2012/04/01
Absorption-spectroscopy
Water-vapor
Temperature Distributions
Gas Temperature
Combustion
Cavity
Operation
Engines
Model