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Knowledge Management System of Institue of Mechanics, CAS
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Effect of characteristic structure of nested composite hybrid rocket fuel grain on combustion properties
期刊论文
ACTA ASTRONAUTICA, 2024, 卷号: 218, 页码: 269-281
Authors:
Wang RY(王若岩)
;
Lin X(林鑫)
;
Wang ZZ(王泽众)
;
Wu K(吴坤)
;
Pan JJ(潘俊杰)
;
Zhang ZL(张泽林)
;
Luo JX(罗家枭)
;
Li F(李飞)
;
Yu XL(余西龙)
Favorite
  |  
View/Download:18/0
  |  
Submit date:2024/05/21
Hybrid rocket
Composite fuel grain
Characteristic structure
Radiation image
Combustion properties
Superior Al90Mg10-Based Composite Fuel Grain for a Hybrid Rocket Engine
期刊论文
JOURNAL OF SPACECRAFT AND ROCKETS, 2024, 页码: 9
Authors:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Pan JJ(潘俊杰)
;
Luo JX(罗家枭)
;
Wang RY(王若岩)
;
Zhang ZL(张泽林)
;
Yu XL(余西龙)
Favorite
  |  
View/Download:19/0
  |  
Submit date:2024/05/21
Combustion Efficiency
Emission Spectroscopy
Hybrid Rocket Engines
Paraffin Based Fuels
Regression rate
Aluminium Alloys
3D Printing
D0
22
precipitates strengthened W-Ta-Fe-Ni refractory high-entropy alloy
期刊论文
JOURNAL OF MATERIALS SCIENCE & TECHNOLOGY, 2024, 卷号: 177, 页码: 85-95
Authors:
Li T(李统)
;
Chen JX(陈金玺)
;
Liu TW(刘天威)
;
Chen Y(陈艳)
;
Luan, Jun-Hua
;
Jiao, Zeng-Bao
;
Liu, Chain-Tsuan
;
Dai LH(戴兰宏)
Favorite
  |  
View/Download:154/0
  |  
Submit date:2024/01/02
Refractory high entropy alloy
Multi-phase structure
D0(22) superlattice
Precipitation strengthening
Regression Rate and Combustion Efficiency of Composite Hybrid Rocket Grains Based on Modular Fuel Units
期刊论文
AEROSPACE, 2024, 卷号: 11, 期号: 4, 页码: 18
Authors:
Pan JJ(潘俊杰)
;
Lin X(林鑫)
;
Wang ZZ(王泽众)
;
Wang RY(王若岩)
;
Wu K(吴坤)
;
Liang, Jinhu
;
Yu XL(余西龙)
Favorite
  |  
View/Download:7/0
  |  
Submit date:2024/05/27
modular unit
modification
regression rate
combustion efficiency
hybrid rocket engine
Multidimensional high-temperature field measurement method for flame based on near infrared radiation spectrum of water vapor
期刊论文
OPTICS AND LASERS IN ENGINEERING, 2024, 卷号: 174, 页码: 13
Authors:
Zhou GX(周功喜)
;
Wang, Wenjie
;
Li F(李飞)
;
Lin X(林鑫)
;
Meng DD(孟东东)
;
Yu XL(余西龙)
Favorite
  |  
View/Download:151/0
  |  
Submit date:2024/02/05
Multi-dimension
High-temperature
Self-Absorption
Reconstruction algorithm
Tailoring nanoprecipitates to achieve ultrahigh strength (CoCrNi)94.5W3Ta2.5 medium-entropy alloys
期刊论文
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2024, 卷号: 892, 页码: 13
Authors:
Chen JX(陈金玺)
;
Li T(李统)
;
Tan YY(谭园园)
;
Chen Y(陈艳)
;
Wang HY(汪海英)
;
Dai LH(戴兰宏)
Favorite
  |  
View/Download:43/0
  |  
Submit date:2024/03/25
Evolution of weakly unstable oblique detonation in disturbed inflow
期刊论文
PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 1, 页码: 12
Authors:
Niu, Shuzhen
;
Yang PF(杨鹏飞)
;
Xi, Xuechen
;
Li, Zhenzhen
;
Teng, Honghui
Favorite
  |  
View/Download:35/0
  |  
Submit date:2024/04/15
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)
Adobe PDF(4980Kb)
  |  
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  |  
View/Download:183/5
  |  
Submit date:2023/09/05
Hybrid rocket engine
additive manufacturing
three-dimensional printing
breathable blade
composite fuel grain
mechanical and combustion properties
porous structure
>
Spectral insight into the interface evolution of a carbon/carbon composite under high-enthalpy, nonequilibrium flow
期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 10, 页码: 13
Authors:
Fang SH(方思晗)
;
Lin X(林鑫)
;
Yang JN(杨俊娜)
;
Zeng, Hui
;
Zhu, Xingying
;
Zhou, Fa
;
Ou, Dongbin
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(4126Kb)
  |  
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  |  
View/Download:61/10
  |  
Submit date:2024/02/26
Combustion Characteristics of a Swirl-Radial-Injection Composite Fuel Grain with Applications in Hybrid Rockets
期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 9, 页码: 19
Authors:
Wang RY(王若岩)
;
Lin X(林鑫)
;
Wang ZZ(王泽众)
;
Wu K(吴坤)
;
Zhang ZL(张泽林)
;
Luo JX(罗家枭)
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(8125Kb)
  |  
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  |  
View/Download:116/12
  |  
Submit date:2023/10/30
hybrid rocket engine
swirl-radial injection
regression rate
flame images
combustion efficiency