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中国科学院力学研究所机构知识库
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张新宇 [9]
陈立红 [7]
仲峰泉 [6]
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航空煤油冲击射流强化传热的实验研究
会议论文
中国航天第三专业信息网第四十届技术交流会暨第四届空天动力联合会议, 中国云南昆明, 2019-08-14
Authors:
杜蒙蒙
;
仲峰泉
;
邢云绯
;
张新宇
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Submit date:2020/09/28
实验研究
冲击射流
航空煤油
强化传热
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
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
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Submit date:2013/04/24
煤油
超临界
对流传热
数值研究
Numerical simulation of ignition and combustion of ethylene in a supersonic model combustor with a reduced kinetic mechanism
期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2013, 卷号: 185, 期号: 4, 页码: 548-563
Authors:
Zhong FQ(仲峰泉)
;
Chen LH(陈立红)
;
Li F(李飞)
;
Zhang XY(张新宇)
;
Sung CJ
;
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:2013/05/03
Ethylene
Ignition
Numerical Simulation
Reduced Kinetic Mechanism
Supersonic Combustion
Numerical investigation on flow and convective heat transfer of aviation kerosene at supercritical conditions
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 2, 页码: 416-422
Authors:
Dang GX(党国鑫)
;
Zhong FQ(仲峰泉)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Zhong, FQ (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:2013/03/04
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
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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
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
Experimental investigation on the cavity-based scramjet model
期刊论文
CHINESE SCIENCE BULLETIN, 2009, 卷号: 54, 期号: 16, 页码: 2794-2799
Authors:
Gu HB(顾洪斌)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Gu HB(顾洪斌)
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View/Download:1153/311
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Submit date:2009/09/28
Scramjet
Combustor
Cavity
Performance