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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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Indexed By:EI
Creator:张新宇
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Document Type:会议论文
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High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model
会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
Authors:
Yang L
;
岳连捷
;
张启帆
;
张新宇
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Submit date:2021/01/12
Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Cheng LW(程柳维)
;
Zhong FQ(仲峰泉)
;
Wang ZP(王知溥)
;
Gu HB(顾洪斌)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
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Submit date:2018/01/16
Combustors
Cracks
Diesel Engines
Efficiency
Ethylene
Fighter Aircraft
Fuels
High Speed Cameras
Ignition
Kerosene
Luminance
Spacecraft
Stabilization
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)
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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)
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Submit date:2018/01/16
Boundary Layer Flow
Boundary Layers
Spacecraft
Wind Tunnels
Large eddy simulation of ignition and combustion of ethylene/air turbulent jet diffusion flame with reduced kinetic mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Ma SG(马素刚)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Zhong, Fengquan (fzhong@imech.ac.cn)
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Submit date:2017/05/05
Combustion Pro
Cess
Directed Relation Graph
Dynamic Evolution
Fuel Injection Velocities
Kinetic Mechanism
Reduced Mechanisms
Temperature Profiles
Temporal And Spatial Evolutions
Numerical study of conjugate heat transfer of supercritical kerosene flow in rectangular cooling channel
会议论文
15th International Heat Transfer Conference, IHTC 2014, Kyoto, Japan, August 10, 2014 - August 15, 2014
Authors:
Zhong FQ(仲峰泉)
;
Dang GX(党国鑫)
;
Xing YF(邢云绯)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Zhong, Fengquan (fzhong@imech.ac.cn)
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Submit date:2017/05/27
Conjugate Heat Transfer
Heat Conduction Equations
Numerical Study
Pseudo-critical Temperature
Rectangular Cooling Channels
Supercritical Kerosenes
Thermodynamic And Transport Properties
Turbulent Transports
Combined TDLAS and OES technique for CO concentration measurement in shock-heated Martian atmosphere
会议论文
2nd International Symposium on Laser Interaction with Matter (LIMIS), Xian, PEOPLES R CHINA, SEP 09-12, 2012
Authors:
Lin X(林鑫)
;
Yu XL(余西龙)
;
Li F(李飞)
;
Zhang SH(张少华)
;
Xin JG
;
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.
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Submit date:2013/12/12
Optical Emission Spectroscopy (Oes)
Tunable Diode Laser Absorption Spectroscopy (Tdlas)
Shock Wave
Temperature
Concentration
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)
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Submit date:2014/02/24
Three-Dimensional heat transfer analysis and optimized design of actively cooled strut for scramjet applications
会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United states, JUL 30-AUG 01, 2012
Authors:
Zhong FQ(仲峰泉)
;
Chen TY(陈同银)
;
Fan XJ(范学军)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Zhong FQ(仲峰泉)
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Submit date:2014/02/24
Modeling and measurements of heat release distributions in dual-mode scramjet 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:
Tian L(田璐)
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Li F(李飞)
;
Zhang XY(张新宇)
;
Tian L(田璐)
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Submit date:2014/02/24