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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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力学所知识产出(19... [2]
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岳连捷 [11]
张启帆 [3]
张旭 [3]
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Numerical study of periodic flame flashback in a cavity-based scramjet combustor
期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 4, 页码: 45108
Authors:
Guo SZ(郭升祖)
;
Zhang X(张旭)
;
Liu QL(刘起立)
;
Yue LJ(岳连捷)
Adobe PDF(5835Kb)
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Submit date:2023/06/15
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet
期刊论文
JOURNAL OF PROPULSION AND POWER, 2023, 页码: 18
Authors:
Yao W(姚卫)
;
Liu H(刘杭)
;
Zhang Z(张政)
;
Zhang X(张旭)
;
Yue LJ(岳连捷)
;
Zhang XY(张晓源)
;
Li JP(李进平)
Adobe PDF(689Kb)
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Submit date:2023/02/27
Numerical study on wave configuration of wedge-induced oblique detonation wave: Reactive boundary layer effect
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 11, 页码: 11
Authors:
Yang L(杨理)
;
Yue LJ(岳连捷)
;
Yu, Dehai
;
Chen, Zheng
Adobe PDF(4548Kb)
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Submit date:2022/12/29
Lagrange Optimization of Shock Waves for Two-Dimensional Hypersonic Inlet with Geometric Constraints
期刊论文
AEROSPACE, 2022, 卷号: 9, 期号: 10, 页码: 15
Authors:
Li YL(李育凌)
;
Yue LJ(岳连捷)
;
He CM(何成明)
;
Wu WN(邬婉楠)
;
Chen H(陈昊)
Adobe PDF(3520Kb)
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Submit date:2022/11/14
scramjet inlet
Lagrange optimization method
shock configuration
Interaction of a shock train with inherent isentropic waves in a curved isolator
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 6, 页码: 21
Authors:
He LH(贺理浩)
;
Chen H(陈昊)
;
Yue LJ(岳连捷)
;
Zhang QF(张启帆)
;
Wu WN(邬婉楠)
Adobe PDF(8942Kb)
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Submit date:2022/11/28
Jet-Driven Unstart Process of a Hypersonic Inlet with Ramp Mass Injection
期刊论文
AIAA JOURNAL, 2022, 页码: 5
Authors:
Li JJ(李江江)
;
Chen H(陈昊)
;
Tong XT(仝晓通)
;
Gao X
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
Adobe PDF(1812Kb)
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Submit date:2022/05/17
Onset of Oblique Detonation Waves for a Cavity-Based Wedge
期刊论文
AIAA JOURNAL, 2022, 页码: 14
Authors:
Yang, Li
;
Yue LJ(岳连捷)
;
Zhang QF(张启帆)
Adobe PDF(5573Kb)
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Submit date:2022/03/05
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:
Zhou GX(周功喜)
;
Zhang X(张旭)
;
Li JP(李进平)
;
Zhang XY(张晓源)
;
Zhang SZ(张仕忠)
;
Lin X(林鑫)
;
Li F(李飞)
;
Chen H(陈宏)
;
Yue LJ(岳连捷)
;
Yu XL(余西龙)
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Submit date:2021/09/07
High mach number scramjet
Circular cross-section
TDLAS
Multi-view simultaneous imaging
POD
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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Submit date:2022/10/25
Boundary layer combustion
Skin-friction reduction
Supersonic combustion
Scramjet engine
Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance
期刊论文
Combustion Science and Technology, 2007, 卷号: 179, 期号: 10, 页码: 2199-2217
Authors:
Fan XJ(范学军)
;
Yu G(俞刚)
;
Li JG(李建国)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Sung CJ
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Submit date:2009/08/03
Entry Conditions
Kerosene
Supersonic Combustion
Thermal Cracking
Model Combustor
Propulsion
Injection