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Indexed By:EI
Source Publication:AEROSPACE SCIENCE AND TECHNOLOGY
Community:高温气体动力学国家重点实验室
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Advances in plasma-assisted ignition and combustion for combustors of aerospace engines
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:
Li, Mengzhe
;
Wang, Zhikai
;
Xu, Rongguang
;
Zhang, Xiaoliang
;
Chen, Zhitong
;
Wang Q(汪球)
Adobe PDF(8841Kb)
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View/Download:283/109
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Submit date:2021/11/01
Non-equilibrium plasma
Plasma-assisted ignition
Plasma-assisted combustion
Aerospace engine
Combustor
Extreme condition
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:
Yao W(姚卫)
;
Liu H(刘杭)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
Adobe PDF(2954Kb)
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View/Download:290/67
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 21
Authors:
Yang L(杨磊)
;
Ye, Zhengyin
;
Li WH(李文皓)
;
Sun QH(孙泉华)
Adobe PDF(4621Kb)
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View/Download:281/61
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Submit date:2021/11/01
Store separation
Aerodynamic modeling
Interference aerodynamics
Dynamic simulation
Air-launch-to-orbit
Reduction of surface friction drag in scramjet engine by boundary layer combustion
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
Authors:
Xue, Rui
;
Zheng, Xing
;
Yue LJ(岳连捷)
;
Zhang, Qian
;
He, Xin
;
Yang, Jing
;
Weng, Chao
;
Li, Zhihao
Adobe PDF(5483Kb)
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View/Download:148/47
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Submit date:2022/10/25
Boundary layer combustion
Skin-friction reduction
Supersonic combustion
Scramjet engine
Parameter-correlation study on shock-shock interaction using a machine learning method
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247
Authors:
Peng J(彭俊)
;
Luo ZT(罗长童)
;
Han ZJ(韩子健)
;
Hu ZM(胡宗民)
;
Han GL(韩桂来)
;
Jiang ZL(姜宗林)
Adobe PDF(2818Kb)
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Submit date:2021/01/29
Shock-shock interaction
Machine learning
Hypersonic flow
Impinging jet
Genetic programming
Triple point
Aerodynamic principles of shock-induced combustion ramjet engines
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8
Authors:
Ma KF(马凯夫)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(1657Kb)
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View/Download:278/98
  |  
Submit date:2020/08/26
Scramjet engines
Shock-induced combustion ramjet engines
Supersonic combustion
Chapman-Jouguet detonation
A multi-time scale solution strategy for an elastomeric aircraft
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 13
Authors:
Yang L(杨磊)
;
Sun QH(孙泉华)
Adobe PDF(1858Kb)
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View/Download:222/90
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Submit date:2020/08/26
Flight dynamic simulation
Multi-time scale
Elastomeric aircraft
Reduced order models
Store separation
Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
Authors:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(1961Kb)
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Submit date:2020/05/18
Hybrid rocket engine
Paraffin-based fuel
Acrylonitrile-butadiene-styrene
Regression rate
Combustion efficiency
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
Authors:
Wang ZP(王知溥)
;
Li F(李飞)
;
Gu HS
;
Yu XL(余西龙)
;
Zhang XY(张新宇)
;
Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:560/232
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Submit date:2015/06/12
Scramjet
Dual-mode Combustor
Divergent Angle
Cavity Location
Combustion Efficiency
Tdlas