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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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张新宇 [14]
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顾洪斌 [7]
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Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:
Tong XT(仝晓通)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
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Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow
微波增强滑移电弧等离子体辅助超声速燃烧
期刊论文
航空学报, 2020, 卷号: 41, 期号: 2, 页码: 123345
Authors:
孟宇
;
顾洪斌
;
孙文明
;
张新宇
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Submit date:2019/12/16
超燃冲压发动机
超声速燃烧
等离子体助燃
滑移电弧
微波
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 heat transfer deterioration of turbulent supercritical kerosene flow in heated circular tube
期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2015, 卷号: 85, 页码: 1003-1011
Authors:
Dang GX
;
Zhong FQ(仲峰泉)
;
Zhang YJ
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Bei Si Huan Xi Rd 15, Beijing 100190, Peoples R China.
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Submit date:2015/06/12
Supercritical Kerosene
Convective Heat Transfer
Turbulent Flow
Numerical Study
H_2O/CO_2污染对RP-3航空煤油着火特性的影响
期刊论文
推进技术, 2015, 卷号: 36, 期号: 3, 页码: 336-344
Authors:
梁金虎
;
王苏
;
张灿
;
张胜涛
;
岳连捷
;
范秉诚
;
张新宇
;
崔季平
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Submit date:2015/12/25
污染效应
着火延时
煤油
H2o
Co2
激波管
Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 28, 期号: 1, 页码: 72-78
Authors:
Li F(李飞)
;
Yu XL(余西龙)
;
Tong YG(仝颖刚)
;
Shen Y(沈岩)
;
Chen J(陈健)
;
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.
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Submit date:2013/07/30
Scramjet
Kerosene Fuel
Plasma Torch
Ignition
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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Submit date:2014/03/11
Combustion Mode
Scramjet
Artificial Neural Network
Study on Judgment Method of Combustion Mode on Dual-mode Scramjet
期刊论文
Procedia Engineering, 2013, 卷号: 67, 页码: 147-154
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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Submit date:2015/09/24
Scramjet
Artificial Neural Network
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)
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Submit date:2014/02/24
双模态发动机的低马赫数燃烧振荡现象
会议论文
第四届高超声速科技学术会议, 中国海南三亚, 2011
Authors:
李飞
;
李智
;
顾洪斌
;
余西龙
;
陈立红
;
张新宇
Adobe PDF(75Kb)
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Submit date:2012/04/01
超燃冲压发动机
双模态
燃烧诊断
高速纹影
Tdlas