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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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仲峰泉 [2]
岳连捷 [2]
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Indexed By:CSCD
Creator:张新宇
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Date Issued:2015
Community:高温气体动力学国家重点实验室
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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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View/Download:302/98
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Submit date:2016/01/08
Reduced Chemistry
Hydrocarbons
Directed Relation Graph
Ignition Delay Time
双模态发动机的模态鉴别方法
期刊论文
力学学报, 2015, 期号: 3, 页码: 389-397
Authors:
李飞
;
王知溥
;
余西龙
;
顾洪斌
;
陈立红
;
张新宇
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Adobe PDF(3140Kb)
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View/Download:459/82
  |  
Submit date:2015/12/25
双模态冲压发动机
模态鉴别
释热分布
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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View/Download:248/65
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Submit date:2015/12/25
污染效应
着火延时
煤油
H2o
Co2
激波管
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
高超声速进气道快速破膜开启的流动特性
期刊论文
航空学报, 2015, 卷号: 36, 期号: 6, 页码: 1795-1804
Authors:
徐骁
;
岳连捷
;
卢洪波
;
肖雅彬
;
张新宇
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View/Download:327/76
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Submit date:2015/12/25
高超声速进气道
破膜开启
非定常效应
激波边界层相互作用
分离流