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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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姜宗林 [3]
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Funding Organization:National Natural Science Foundation of China
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Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition
期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
Authors:
Zhang WS(张文硕)
;
Zhang, Zijian
;
Jiang ZL(姜宗林)
;
Han X(韩信)
;
Liu YF(刘云峰)
;
Wang C(王春)
Adobe PDF(15045Kb)
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View/Download:267/30
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Submit date:2022/01/24
Near-field relaxation subsequent to the onset of oblique detonations with a two-step kinetic model
期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 9, 页码: 11
Authors:
Teng, Honghui
;
Ng, Hoi Dick
;
Yang PF(杨鹏飞)
;
Wang, Kuanliang
Adobe PDF(5463Kb)
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View/Download:185/36
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Submit date:2022/01/13
Characterizing combustion of a hybrid rocket using laser absorption spectroscopy
期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2021, 卷号: 127, 页码: 9
Authors:
Fang SH(方思晗)
;
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Li RJ(李仁杰)
;
Li, Jing
;
Zhang, Zhedian
;
Liu, Yan
;
Yu XL(余西龙)
Adobe PDF(4367Kb)
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View/Download:556/72
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Submit date:2021/08/03
Tunable diode laser absorption spectroscopy
Hybrid rocket motor
Temperature
Partial pressure
Combustion efficiency
Reconstructing shock front of unstable detonations based on multi-layer perceptron
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
Authors:
Zhou, Lin
;
Teng, Honghui
;
Ng, Hoi Dick
;
Yang PF(杨鹏飞)
;
Jiang ZL(姜宗林)
Adobe PDF(6382Kb)
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View/Download:241/37
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Submit date:2021/11/01
Cellular detonation
Lead shock evolution
Multi-layer perceptron
Numerical simulations
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)
Adobe PDF(4108Kb)
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View/Download:344/53
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Submit date:2021/09/07
High mach number scramjet
Circular cross-section
TDLAS
Multi-view simultaneous imaging
POD
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:
Tong XT(仝晓通)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(8067Kb)
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View/Download:413/75
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Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow
Formation of stabilized oblique detonation waves in a combustor
期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors:
Zhang ZJ(张子健)
;
Wen, Chihyung
;
Zhang WS(张文硕)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(3599Kb)
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Submit date:2021/03/03
Oblique detonation wave
Combustor
Oblique detonation engine
Normal detonation wave
Boundary layer separation
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
Effects of boundary layer on wedge-induced oblique detonation structures in hydrogen-air mixtures
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2019, 卷号: 44, 期号: 41, 页码: 23429-23435
Authors:
Fang YS(方宜申)
;
Zhang ZJ(张子健)
;
Hu ZM(胡宗民)
Adobe PDF(1085Kb)
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Submit date:2019/10/21
Oblique detonation wave
Boundary layer
Viscosity
Detonation initiation
Hydrogen-air mixture