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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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Effect of pilot hydrogen on the mixing and combustion characteristics in kerosene-fueled scramjet
期刊论文
APPLIED THERMAL ENGINEERING, 2025, 卷号: 258, 页码: 10./通讯作者:Tian, Zhen-Yu
Authors:
Shi, HongQing
;
Wang, Du
;
Cui NF(崔乃夫)
;
Zhao, ChenYang
;
Lei, JieMing
;
Zhu, ZiQiang
;
Zhang, YaNing
;
Tian, ZhenYu
Favorite
  |  
View/Download:11/0
  |  
Submit date:2024/11/22
Scramjet
Pilot hydrogen
Dual cavities
Mixing efficiency
Combustion performance
Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11./通讯作者:Sun, Mingbo, Zhao, Guoyan
Authors:
Liu, Mingjiang
;
Sun, Mingbo
;
Zhao, Guoyan
;
Meng Y(孟宇)
;
Huang, Yuhui
;
Ma, Guangwei
;
Wang, Hongbo
Adobe PDF(3841Kb)
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View/Download:186/41
  |  
Submit date:2022/12/20
Tandem-cavity
Scramjet combustor
Combustion mode
Thrust performance
Effect of helical fins on the combustion performance in a micro-step combustor
期刊论文
FUEL, 2022, 卷号: 319, 页码: 13./通讯作者:Yao, Wei
Authors:
Zhang Z(张政)
;
Shen WBY
;
Yao W(姚卫)
;
Wang Q(汪球)
;
Zhao W(赵伟)
Adobe PDF(11881Kb)
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View/Download:386/60
  |  
Submit date:2022/05/17
Micro-combustion
Helical fin
Combustion performance
Conjugate heat transfer
Mixing
Enhancement of combustion performance in a microchannel: Synergistic effects of bluff-body and cavity
期刊论文
FUEL, 2020, 卷号: 265, 页码: 11./通讯作者:Wang, Jian
Authors:
Zhang Z
;
Wu K(吴坤)
;
Yao W(姚卫)
;
Yuen R
;
Wang J
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  |  
Adobe PDF(3821Kb)
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View/Download:458/130
  |  
Submit date:2020/04/07
Micro-combustor
Bluff-body
Cavity
Combustion performance
Flame-flow interaction
Development of the facility for model scramjet testing
会议论文
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japan, April 24, 2001 - April 27, 2001
Authors:
Chang XY(张新宇)
;
Chen LH(陈立红)
;
Yu G(俞刚)
;
Qian DX(钱大兴)
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  |  
Adobe PDF(872Kb)
  |  
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View/Download:289/103
  |  
Submit date:2017/06/01
Chinese Academy Of Sciences
Enthalpy Flow
Hypersonic Propulsion Test Facility
Performance Tests
Scramjet Testing
Supersonic Combustion
Total Pressure
Total Temperatures
Combustion of kerosene in a supersonic stream
会议论文
38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United states, January 10, 2000 - January 13, 2000
Authors:
Li JG(李建国)
;
Yu G(俞刚)
;
Zhang XY(张新宇)
;
Huang QS
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  |  
Adobe PDF(519Kb)
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View/Download:251/127
  |  
Submit date:2017/06/01
Cavity Flame Holders
Combustion Efficiencies
Combustor Performance
Equivalence Ratios
Modular Structures
Optimized Conditions
Stagnation Pressures
Supersonic Combustors