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Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet
期刊论文
JOURNAL OF PROPULSION AND POWER, 2024, 页码: 17
作者:
Liu H(刘杭)
;
Yao W(姚卫)
;
Zhang X(张旭)
;
Zhang XY(张晓源)
;
Liu, Jianwen
收藏
  |  
浏览/下载:1/0
  |  
提交时间:2024/03/11
Scramjet
Dynamic Zone Flamelet Model
High Enthalpy Shock Tunnel
Combustors
Improved Delayed Detached Eddy Simulation
Vibrational Energy
nonequilibrium heating
cooling effects
thermal nonequilibrium
chemical nonequilibrium
hydrogen
Study on heat transfer coupling mechanism of direct thermoelectric conversion with regenerative cooling for supersonic combustor applications
期刊论文
APPLIED THERMAL ENGINEERING, 2024, 卷号: 238, 页码: 15
作者:
Gao EK(高尔康)
;
Zhong FQ(仲峰泉)
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  |  
浏览/下载:0/0
  |  
提交时间:2024/02/26
Direct thermoelectric conversion
Regenerative cooling
Supersonic combustor
Analytical model
Genetic algorithm
Standing oblique detonation for hypersonic propulsion: A review
期刊论文
PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17
作者:
Jiang ZL(姜宗林)
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  |  
浏览/下载:0/0
  |  
提交时间:2024/02/26
Standing oblique detonation
Scramjet engine
Oblique detonation engine
Shock wave
Supersonic combustion
Hypersonic ramjet propulsion
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
作者:
Zhang Z(张政)
;
Shen WBY
;
Yao W(姚卫)
;
Wang Q(汪球)
;
Zhao W(赵伟)
收藏
  |  
浏览/下载:34/0
  |  
提交时间:2022/05/17
Micro-combustion
Helical fin
Combustion performance
Conjugate heat transfer
Mixing
Investigation for Effects of Jet Scale on Flame Stabilization in Scramjet Combustor
期刊论文
ENERGIES, 2022, 卷号: 15, 期号: 10, 页码: 16
作者:
Li, Zhen
;
Gu, Hongbin
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  |  
浏览/下载:15/0
  |  
提交时间:2022/07/18
scramjet combustor
direct-connect test
jet scale
flame stabilization
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
作者:
Li, Mengzhe
;
Wang, Zhikai
;
Xu, Rongguang
;
Zhang, Xiaoliang
;
Chen, Zhitong
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  |  
浏览/下载:40/0
  |  
提交时间:2021/11/01
Non-equilibrium plasma
Plasma-assisted ignition
Plasma-assisted combustion
Aerospace engine
Combustor
Extreme condition
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
作者:
Teng, Honghui
;
Ng, Hoi Dick
;
Yang PF(杨鹏飞)
;
Wang, Kuanliang
收藏
  |  
浏览/下载:10/0
  |  
提交时间:2022/01/13
Reconstruction model for heat release rate based on artificial neural network
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 37, 2021, 卷号: 46, 页码: 19599-19616
作者:
Li B(李波)
;
Yao W(姚卫)
;
Li YC(李亚超)
;
Fan XJ(范学军)
收藏
  |  
浏览/下载:98/0
  |  
提交时间:2022/10/25
Heat release rate (HRR)
Artificial neural network (ANN)
Proper orthogonal -12omposition (POD)
Chemiluminescence
Supersonic hydrogen flame
Criteria for hypersonic airbreathing propulsion and its experimental verification
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
作者:
Jiang ZL(姜宗林)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Wang C(王春)
;
Luo ZT(罗长童)
收藏
  |  
浏览/下载:50/0
  |  
提交时间:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
Evaporation and Combustion Characteristics of Kerosene Droplets in Localized Stratified Vortex-tube Combustor: A Numerical Investigation
期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2020, 页码: 16
作者:
Ren, Shoujun
;
Wang, Xiaohan
;
Jiang, Liqiao
收藏
  |  
浏览/下载:13/0
  |  
提交时间:2021/10/22
Vortex-tube combustor
AC(10)H(20)droplet
evaporation ratio
flame structure
combustion characteristic
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