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Knowledge Management System of Institue of Mechanics, CAS
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State Key... [16]
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张新宇 [16]
陈立红 [9]
仲峰泉 [5]
岳连捷 [5]
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Language:英语
Document Type:会议论文
Author:张新宇
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Community:高温气体动力学国家重点实验室
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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
Numerical Study of Heat Transfer on Confined Under-Expanded Impinging Jet from Slot into a Plenum
会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
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Submit date:2023/03/17
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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View/Download:288/98
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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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View/Download:348/76
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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
Study on Judgment Method of Combustion Mode on Dual-mode Scramjet
会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
Authors:
Chen Q(陈强)
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
;
Wang P
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View/Download:589/190
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Submit date:2014/03/11
Combustion Mode
Scramjet
Artificial Neural Network
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
A coupled heat transfer analysis with effects of thermal/catalytic cracking of kerosene for regenerative cooled supersonic combustor
会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
Authors:
Wang X(王曦)
;
Zhong FQ(仲峰泉)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
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Submit date:2014/04/02
Kerosene
Combustor
Thermal
Regenerative
Coupled
Catalytic
Cracking
Analysis
Supersonic
Transfer
Cooled
Effects
Board
Solving
Extra
Through
Differ
Energy
Cooling
Model