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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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Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades
期刊论文
VIRTUAL AND PHYSICAL PROTOTYPING, 2023, 卷号: 18, 期号: 1, 页码: e2235680
Authors:
Qu DD(屈丹丹)
;
Lin X(林鑫)
;
Zhang K(张坤)
;
Li ZY(李志永)
;
Wang ZZ(王泽众)
;
Liu GL(刘国亮)
;
Meng Y(孟洋)
;
Luo GX(罗耕星)
;
Wang RY(王若岩)
;
Yu XL(余西龙)
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  |  
View/Download:150/0
  |  
Submit date:2023/09/05
Hybrid rocket engine
additive manufacturing
three-dimensional printing
breathable blade
composite fuel grain
mechanical and combustion properties
porous structure
>
Standing oblique detonation for hypersonic propulsion: A review
期刊论文
PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17
Authors:
Jiang ZL(姜宗林)
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View/Download:17/0
  |  
Submit date:2024/02/26
Standing oblique detonation
Scramjet engine
Oblique detonation engine
Shock wave
Supersonic combustion
Hypersonic ramjet propulsion
Analysis of spray characteristics of a jet film injection element based on Voronoi tessellation
期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 206, 页码: 100-113
Authors:
He CM(何成明)
;
Zhang, Peng
;
He, Zhixia
;
Yue LJ(岳连捷)
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  |  
View/Download:41/0
  |  
Submit date:2023/04/20
Liquid rocket engine
Pintle injector
Spray characteristics
Jet film injection
Voronoi tessellation
Effects of swirl injection on the combustion of a 11el composite hybrid rocket fuel grain
期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182
Authors:
Zhang ZL(张泽林)
;
Lin X(林鑫)
;
Wang ZZ(王泽众)
;
Wu K(吴坤)
;
Luo JX(罗家枭)
;
Fang SH(方思晗)
;
Zhang CY
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(9227Kb)
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View/Download:110/27
  |  
Submit date:2022/10/23
Hybrid rocket engine
Swirl injection
11el composite fuel grain
Regression rate
Oxidizer-to-fuel ratio
Three-dimensional printed metal-nested composite fuel grains with superior mechanical and combustion properties
期刊论文
VIRTUAL AND PHYSICAL PROTOTYPING, 2022, 卷号: 17, 期号: 3, 页码: 437-450
Authors:
Lin X(林鑫)
;
Qu DD(屈丹丹)
;
Chen XD(陈雪冬)
;
Wang ZZ(王泽众)
;
Luo JX(罗家枭)
;
Meng DD(孟东东)
;
Liu GL(刘国亮)
;
Zhang K(张坤)
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(3694Kb)
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View/Download:108/24
  |  
Submit date:2022/10/23
Hybrid rocket engine
additive manufacturing
metal-nested composite fuel grain
mechanical properties
combustion properties
optical emission spectroscopy
Parameters for evaluating the efficiency of inlet compression
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors:
Chen KT(陈科挺)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(511Kb)
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  |  
View/Download:186/33
  |  
Submit date:2022/01/12
Airbreathing engine
Compression efficiency
Compression quality
Inlet
Self-consistency
Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy
期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120
Authors:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Peng JL(彭锦龙)
;
Liu, Yan
;
Zhang ZL(张泽林)
;
Fang SH(方思晗)
;
Yu XL(余西龙)
Adobe PDF(6496Kb)
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View/Download:256/45
  |  
Submit date:2021/11/01
Hybrid rocket engine
Fuel mass flow rate
Tunable diode laser absorption spectroscopy
Temperature
Partial pressure
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:256/102
  |  
Submit date:2021/11/01
Non-equilibrium plasma
Plasma-assisted ignition
Plasma-assisted combustion
Aerospace engine
Combustor
Extreme condition
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:115/37
  |  
Submit date:2022/10/25
Boundary layer combustion
Skin-friction reduction
Supersonic combustion
Scramjet engine
Criteria for hypersonic airbreathing propulsion and its experimental verification
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:
Jiang ZL(姜宗林)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Wang C(王春)
;
Luo ZT(罗长童)
Adobe PDF(1806Kb)
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View/Download:269/49
  |  
Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test