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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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仲峰泉 [11]
张新宇 [11]
邢云绯 [5]
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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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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
基于分形几何的超声速燃烧火焰形态表征方法研究
期刊论文
实验流体力学, 2019, 卷号: 33, 期号: 1, 页码: 97-102
Authors:
程柳维
;
仲峰泉
;
杜蒙蒙
;
顾洪斌
;
张新宇
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Submit date:2019/01/09
流量突变条件下煤油流动与对流传热特性实验
期刊论文
航空动力学报, 2018, 卷号: 33, 期号: 5, 页码: 1186-1192
Authors:
张永江
;
仲峰泉
;
邢云绯
;
张新宇
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View/Download:309/72
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Submit date:2018/10/24
流量突变
对流传热
航空煤油
过压液态
摩阻系数
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions
期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:
Tian L
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Chen, LH (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:2016/09/14
Dual-mode Scramjet
Engine Performance
Thrust
Optimization
Heat Release Distribution
Simulated Annealing Algorithm
Development of efficient and accurate skeletal mechanisms for hydrocarbon fuels and kerosene surrogate
期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 5, 页码: 732-740
Authors:
Zhong FQ(仲峰泉)
;
Ma SG
;
Zhang XY(张新宇)
;
Sung CJ
;
Niemeyer KE
;
Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2016/01/08
Reduced Chemistry
Hydrocarbons
Directed Relation Graph
Ignition Delay Time
Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel
期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475
Authors:
Xing YF(邢云绯)
;
Zhong FQ(仲峰泉)
;
Li DX(李东霞)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2015/04/28
Hypersonic Scramjet Test Tunnel
Nozzle
Aerodynamic Heating
Convective Heat Transfer
矩形横截面螺旋管湍流流动与传热特性的数值研究
期刊论文
航空学报, 2013, 卷号: 34, 期号: 6, 页码: 1269-1276
Authors:
邢云绯
;
仲峰泉
;
张新宇
Adobe PDF(894Kb)
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Submit date:2013/07/10
螺旋管
湍流
曲率
传热
矩形
超临界态煤油流动与对流传热特性数值研究
期刊论文
中国科学. 技术科学, 2013, 卷号: 43, 期号: 4, 页码: 440-446
Authors:
党国鑫
;
仲峰泉
;
陈立红
;
张新宇
Adobe PDF(1112Kb)
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View/Download:1476/444
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Submit date:2013/04/24
煤油
超临界
对流传热
数值研究
考虑煤油裂解效应的超声速燃烧室再生冷却过程分析
期刊论文
推进技术, 2013, 卷号: 34, 期号: 1, 页码: 47-53
Authors:
王曦
;
仲峰泉
;
陈立红
;
张新宇
Adobe PDF(779Kb)
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View/Download:1193/385
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Submit date:2013/03/07
超声速燃烧室
耦合传热
再生冷却
超临界态
催化裂解