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科研机构
北京航空航天大学 [5]
工程热物理研究所 [3]
清华大学 [2]
天津大学 [1]
内容类型
期刊论文 [10]
会议论文 [1]
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2019 [1]
2017 [1]
2015 [2]
2014 [1]
2013 [4]
2010 [2]
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浏览/检索结果:
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Failure mechanism of thermal barrier coatings of an ex-service aero-engine combustor
期刊论文
Surface and Coatings Technology, 2019, 页码: 125030
作者:
Huwei Dai
;
Junhong Zhang
;
Yanyan Ren
;
Nuohao Liu
;
Bin Wu
收藏
  |  
浏览/下载:20/0
  |  
提交时间:2019/11/21
Thermal barrier coatings (TBCs)
Aero-engine combustor
Premature spallation
Failure mechanism
Influence of coupled characteristics on the internally-staged combustor under low-power operation
期刊论文
Hangkong Dongli Xuebao/Journal of Aerospace Power, 2017, 卷号: 32, 页码: 42-52
作者:
Kang, Y.
;
Lin, Y.-Z.
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  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Aircraft engines
Blowouts
Combustion
Combustors
Efficiency
Flow fields
Nitrogen oxides
Aero-engine
Combustion performance
Coupled characteristics
Staged combustor
Step height
Optical properties
A Hybrid Semi-empirical Model for Lean Blow-Out Limit Predictions of Aero-engine Combustors
期刊论文
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2015, 卷号: 137, 期号: 3
作者:
Hu, Bin
;
Huang, Yong
;
Xu, Jianzhong
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  |  
浏览/下载:13/0
  |  
提交时间:2015/10/27
numerical simulation
lean blow-out
aero-engine combustor
nonreacting flow
hybrid model
A Hybrid Semi-empirical Model for Lean Blow-Out Limit Predictions of Aero-engine Combustors
期刊论文
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2015, 卷号: 137
作者:
Hu, Bin
;
Huang, Yong
;
Xu, Jianzhong
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2020/01/06
numerical simulation
lean blow-out
aero-engine combustor
nonreacting flow
hybrid model
A HYBRID SEMI-EMPIRICAL MODEL FOR LEAN BLOW-OUT LIMIT PREDICTIONS OF AERO-ENGINE COMBUSTORS
会议论文
PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 4B, 2014-01-01
作者:
Hu, Bin
;
Huang, Yong
;
Xu, Jianzhong
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  |  
浏览/下载:4/0
  |  
提交时间:2020/01/06
numerical simulation
lean blow-out
aero-engine combustor
non-reacting flow
hybrid model
FIA method for LBO limit predictions of aero-engine combustors based on FV model
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 28, 期号: 1, 页码: 435-446
作者:
Hu, Bin
;
Huang, Yong
;
Wang, Fang
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  |  
浏览/下载:36/0
  |  
提交时间:2015/10/23
Aero-engine combustor
Lean blow out
Fuel iterative approximation
Flame volume
Numerical simulation
CFD predictions of LBO limits for aero-engine combustors using fuel iterative approximation
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 1, 页码: 74-84
作者:
Hu Bin
;
Huang Yong
;
Wang Fang
;
Xie Fa
收藏
  |  
浏览/下载:17/0
  |  
提交时间:2015/10/27
Aero-engine combustor
Computational fluid dynamics
Fuel iterative approximation
LBO limits prediction
Perfect stirred reactor
FIA method for LBO limit predictions of aero-engine combustors based on FV model
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 28, 页码: 435-446
作者:
Hu, Bin
;
Huang, Yong
;
Wang, Fang
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2020/01/06
Aero-engine combustor
Lean blow out
Fuel iterative approximation
Flame volume
Numerical simulation
CFD predictions of LBO limits for aero-engine combustors using fuel iterative approximation
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 页码: 74-84
作者:
Hu Bin
;
Huang Yong
;
Wang Fang
;
Xie Fa
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2020/01/06
Aero-engine combustor
Computational fluid dynamics
Fuel iterative approximation
LBO limits prediction
Perfect stirred reactor
Combustion and cooling performance in an aero-engine annular combustor
期刊论文
2010, 2010
Peng, X.F.
;
Li, L.
;
Liu, T.
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  |  
浏览/下载:3/0
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