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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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Indexed By:SCI
Source Publication:AEROSPACE SCIENCE AND TECHNOLOGY
Funding Organization:National Natural Science Foundation of China
Community:高温气体动力学国家重点实验室
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Aerodynamic optimization of hypersonic blunted waveriders based on symbolic regression
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 18
Authors:
Guo SQ(郭帅旗)
;
Liu W(刘文)
;
Zhang CA(张陈安)
;
Liu Y(刘洋)
;
Wang FM(王发民)
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View/Download:34/0
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Submit date:2024/02/05
Hypersonic waverider
Aerodynamic model
Symbolic regression
Bluntness effect
Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
Authors:
Zhang ZJ(张子健)
;
Ma KF(马凯夫)
;
Zhang WS(张文硕)
;
Han X(韩鑫)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(2608Kb)
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Submit date:2020/11/30
Oblique detonation engine
Pre-injection
Detonative combustion
Mixing
Hydrogen
Numerical study on the shock/combustion interaction of oblique detonation waves
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
Authors:
Yang L
;
Yue LJ(岳连捷)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
Adobe PDF(5176Kb)
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Submit date:2020/11/30
Oblique detonation wave
Shock/combustion interaction
Shock polar analysis
High-resolution simulation
Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781
Authors:
Zhong FQ(仲峰泉)
;
Cheng LW(程柳维)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
Adobe PDF(2032Kb)
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Submit date:2019/05/29
Supersonic combustor
Hydrocarbon
Mixture fuel
Flame structure
Ignition