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Rui Xue
Rui Xue
在 xjtu.edu.cn 的电子邮件经过验证
标题
引用次数
引用次数
年份
Combustion oscillation study in a kerosene fueled rocket-based combined-cycle engine combustor
ZW Huang, GQ He, F Qin, R Xue, XG Wei, L Shi
Acta Astronautica 129, 260-270, 2016
432016
Effect of steam addition on gas turbine combustor design and performance
R Xue, C Hu, V Sethi, T Nikolaidis, P Pilidis
Applied Thermal Engineering 104, 249-257, 2016
332016
Experimental study on combustion modes of a liquid kerosene fueled RBCC combustor
R Xue, G He, X Wei, C Hu, X Tang, C Weng
Fuel 197, 433-444, 2017
302017
Numerical investigation of combustion field of hypervelocity scramjet engine
S Zhang, J Li, F Qin, Z Huang, R Xue
Acta Astronautica 129, 357-366, 2016
302016
A novel cathode gas diffusion layer for water management of passive μ-DMFC
R Xue, Y Zhang, X Liu
Energy 139, 535-541, 2017
282017
Effect of parallel-jet addition on the shock train characteristics in a central-strut isolator by detached eddy simulation
R Xue, X Wei, G He, C Hu, X Tang
International Journal of Heat and Mass Transfer 114, 1159-1168, 2017
202017
Study on the mechanism of shock wave and boundary layer interaction control using high-frequency pulsed arc discharge plasma
X Ma, J Fan, Y Wu, X Liu, R Xue
Physics of Fluids 34 (8), 2022
182022
Reduction of surface friction drag in scramjet engine by boundary layer combustion
R Xue, X Zheng, L Yue, Q Zhang, X He, J Yang, C Weng, Z Li
Aerospace Science and Technology 115, 106788, 2021
182021
Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion
R Xue, X Zheng, L Yue, S Zhang, C Weng
Acta Astronautica 174, 11-23, 2020
182020
Study on transient process of mode transition in a scramjet combustor with pilot hydrogen
R Xue, M Xu, C Bai, C Weng, C Xu
International Journal of Energy Research 42 (7), 2481-2493, 2018
182018
rGO deposited in stainless steel fiber felt as mass transfer barrier layer for μ-DMFC
Y Zhang, R Xue, X Zhang, J Song, X Liu
Energy 91, 1081-1086, 2015
162015
Investigation on burning behaviors of aluminum agglomerates in solid rocket motor with detailed combustion model
X Zou, N Wang, L Han, R Xue, C Xu, W Zhuang, B Shi
Acta Astronautica 206, 243-256, 2023
132023
Research on shock wave characteristics in the isolator of central strut rocket-based combined cycle engine under Ma5. 5
X Wei, R Xue, F Qin, C Hu, G He
Acta Astronautica 140, 284-292, 2017
132017
Study on the flow field of a kerosene-fueled integrated inlet-combustor-nozzle oblique detonation engine
P Du, R Xue, Y Wu, J Liu
Physics of Fluids 35 (6), 2023
122023
Flow control effect of pulsed arc discharge plasma actuation on impinging shock wave/boundary layer interaction
X Ma, J Fan, Y Wu, S Zhu, R Xue
Physics of Fluids 35 (3), 2023
122023
Combustion flow field analysis of a scramjet engine at high Mach number
RX S.-K. Zhang, J. Li, Z.-W. Huang, F. Qin
Journal of Astronautics 38 (1), 80-88, 2017
122017
Numerical simulation of the interaction between shock train and combustion in three-dimensional M12-02 scramjet model
Y Liu, X He, R Xue, Y Zhang, C Xu, J Du
International Journal of Hydrogen Energy 47 (12), 8026-8036, 2022
112022
Numerical simulation on the shock wave focusing detonation process in the semicircle reflector
P Du, R Xue, Z Yang, B Liu, S Zhu
Physics of Fluids 35 (2), 2023
102023
RBCC constant dynamic pressure booster trajectory design and propellant mass flowrate analysis for TSTO transportation system
X Rui, H Chunbo, L Xiang
Journal of Solid Rocket Technology 36 (2), 155-160, 2013
102013
Response characteristics of impinging shock wave/turbulent boundary layer interaction disturbed by arc plasma energy deposition
L Feng, X Ma, Y Zhang, C Wang, R Xue, Z Chen
Physics of Fluids 34 (1), 2022
92022
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