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滕宏辉 [10]
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Effects of injection parameters on propagation patterns of hydrogen-fueled rotating detonation waves
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2022, 卷号: 47, 期号: 91, 页码: 38811-38822
Authors:
Yao KP(姚克鹏)
;
Yang PF(杨鹏飞)
;
Teng, Honghui
;
Chen, Zheng
;
Wang C(王春)
Adobe PDF(3824Kb)
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Submit date:2022/12/20
Rotating detonation wave
Incomplete mixing
Injection parameters
Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet
期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 193, 页码: 237-254
Authors:
Dai, Chunliang
;
Sun, Bo
;
Zhou, Shengbing
;
Zhuo, Changfei
;
Zhou, Changsheng
;
Yue LJ(岳连捷)
Adobe PDF(13791Kb)
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Submit date:2022/05/17
Mach 12 scramjet inlet
High temperature
Non-equilibrium effects
Thermochemical
Inlet performance
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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Submit date:2022/01/24
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:
Li, Mengzhe
;
Wang, Zhikai
;
Xu, Rongguang
;
Zhang, Xiaoliang
;
Chen, Zhitong
;
Wang Q(汪球)
Adobe PDF(8841Kb)
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Submit date:2021/11/01
Non-equilibrium plasma
Plasma-assisted ignition
Plasma-assisted combustion
Aerospace engine
Combustor
Extreme condition
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:
Yao W(姚卫)
;
Liu H(刘杭)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
Adobe PDF(2954Kb)
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
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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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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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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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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Submit date:2021/09/07
High mach number scramjet
Circular cross-section
TDLAS
Multi-view simultaneous imaging
POD
Numerical and experimental study on high-speed hydrogen-oxygen combustion gas flow and aerodynamic heating characteristics
期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 7, 页码: 11
Authors:
Yu JP(于江鹏)
;
Li JP(李进平)
;
Wang Q(汪球)
;
Zhang SZ(张仕忠)
;
Zhang XY(张晓源)
Adobe PDF(3271Kb)
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Submit date:2021/11/01