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张新宇 [6]
仲峰泉 [3]
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Creator:张新宇
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Document Type:会议论文
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
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
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
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
Performance of the fuel injector in supersonic combustor
会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009
Authors:
Wei Z(卫喆)
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Li F(李飞)
;
Gu SL(顾声龙)
;
Chang XY(张新宇)
;
Wei, Z. (weizhejiji@yahoo.com.cn)
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Submit date:2017/07/14
Concentration Profiles
Engine Design
Fuel Injectors
Fuel-air Mixing
Gas Sampling
Ramp Injector
Scramjet Combustors
Scramjet Test
Supersonic Combustors