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 | 43 | 2016 |
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 | 33 | 2016 |
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 | 30 | 2017 |
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 | 30 | 2016 |
A novel cathode gas diffusion layer for water management of passive μ-DMFC R Xue, Y Zhang, X Liu Energy 139, 535-541, 2017 | 28 | 2017 |
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 | 20 | 2017 |
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 | 18 | 2022 |
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 | 18 | 2021 |
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 | 18 | 2020 |
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 | 18 | 2018 |
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 | 16 | 2015 |
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 | 13 | 2023 |
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 | 13 | 2017 |
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 | 12 | 2023 |
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 | 12 | 2023 |
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 | 12 | 2017 |
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 | 11 | 2022 |
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 | 10 | 2023 |
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 | 10 | 2013 |
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 | 9 | 2022 |