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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 [5]
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Indexed By:CSCD
Creator:张新宇
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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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Submit date:2021/03/30
Adverse pressure gradient
Back pressure
Hysteresis effects
Non-uniform flow
Shock train
Study of coupled effect of impingement jet cooling of kerosene with solid structure
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2019, 卷号: 62, 期号: 11, 页码: 2021-2028
Authors:
Du MM(杜蒙蒙)
;
Zhong FQ(仲峰泉)
;
Xing YF(邢云绯)
;
Zhang XY(张新宇)
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View/Download:373/92
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Submit date:2020/03/21
impingement jet cooling
hydrocarbon fuel
heat transfer enhancement
fluid-solid coupling
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
洛仑兹力控制高超声速进气道边界层分离的数值模拟
期刊论文
推进技术, 2011, 卷号: 32, 期号: 1, 页码: 36-41
Authors:
苏纬仪
;
张新宇
;
张堃元
Adobe PDF(293Kb)
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View/Download:719/185
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Submit date:2012/04/01
高超声速进气道
Mhd流动控制
激波-边界层相互作用
边界层分离
数值仿真
MHD控制激波诱导湍流边界层分离的机理分析
期刊论文
推进技术, 2010, 卷号: 31, 期号: 1, 页码: 18-23
Authors:
苏纬仪
;
陈立红
;
张新宇
Adobe PDF(285Kb)
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Submit date:2010/05/03
激波边界层相互作用
Mhd流动控制
小磁雷诺数
边界层分离