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岳连捷 [10]
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Experimental investigation of mode transition process in a cavity-based scramjet
期刊论文
PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 4, 页码: 11
Authors:
Meng Y(孟宇)
;
Sun WM(孙文明)
;
Gu HB(顾洪斌)
;
Chen, Fang
Favorite
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View/Download:16/0
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Submit date:2024/05/14
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
Authors:
Liu H(刘杭)
;
Yao W(姚卫)
;
Zhang X(张旭)
;
Zhang XY(张晓源)
;
Liu, Jianwen
;
Yue LJ(岳连捷)
;
Sun QH(孙泉华)
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View/Download:56/0
  |  
Submit date: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
Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11
Authors:
Liu, Mingjiang
;
Sun, Mingbo
;
Zhao, Guoyan
;
Meng Y(孟宇)
;
Huang, Yuhui
;
Ma, Guangwei
;
Wang, Hongbo
Adobe PDF(3841Kb)
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  |  
Submit date:2022/12/20
Tandem-cavity
Scramjet combustor
Combustion mode
Thrust performance
Experimental Investigation of Abrupt Change in a Scramjet with Variable Mach-Number Flow
期刊论文
AIAA JOURNAL, 2022, 页码: 9
Authors:
Wu ZJ(吴振杰)
;
Zhang QF(张启帆)
;
Zhang X(张旭)
;
Luo WH(罗苇航)
;
Gao ZB(高占彪)
;
Yue LJ(岳连捷)
Adobe PDF(3049Kb)
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  |  
Submit date:2022/07/18
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
Authors:
Li Z(李桢)
;
Gu HB(顾洪斌)
Adobe PDF(7637Kb)
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View/Download:264/122
  |  
Submit date:2022/07/18
scramjet combustor
direct-connect test
jet scale
flame stabilization
Improved delayed detached eddy simulation of supersonic combustion fueled by liquid kerosene
期刊论文
FUEL, 2022, 卷号: 313, 页码: 13
Authors:
Shen, Wubingyi
;
Huang, Yue
;
Yao W(姚卫)
;
Liu, Hedong
;
You, Yancheng
Adobe PDF(9915Kb)
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View/Download:192/46
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Submit date:2022/05/17
Improved delayed detached eddy simulation
Liquid kerosene
Skeletal reaction mechanism
Equivalence ratio
Cavity-based scramjet combustor
Supersonic combustion
Fuel Regulation Historical Effects on Flame Stabilizations in a Cavity-Based Scramjet Combustor
期刊论文
AIAA JOURNAL, 2022, 页码: 7
Authors:
Zhang X(张旭)
;
Zhang QF(张启帆)
;
Wu ZJ(吴振杰)
;
Yue LJ(岳连捷)
;
Gao ZB(高占彪)
;
Luo WH(罗苇航)
;
Chen H(陈昊)
Adobe PDF(1382Kb)
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View/Download:164/32
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Submit date:2022/03/22
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
Error Analysis of Integrated Absorbance for TDLAS in a Nonuniform Flow Field
期刊论文
APPLIED SCIENCES-BASEL, 2021, 卷号: 11, 期号: 22, 页码: 15
Authors:
Li RJ(李仁杰)
;
Li F(李飞)
;
Lin X(林鑫)
;
Yu XL(余西龙)
Adobe PDF(7410Kb)
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Submit date:2022/01/13
TDLAS
integrated absorbance
error analysis
Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy
期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120
Authors:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Peng JL(彭锦龙)
;
Liu, Yan
;
Zhang ZL(张泽林)
;
Fang SH(方思晗)
;
Yu XL(余西龙)
Adobe PDF(6496Kb)
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Submit date:2021/11/01
Hybrid rocket engine
Fuel mass flow rate
Tunable diode laser absorption spectroscopy
Temperature
Partial pressure