| Intermittent back-flash phenomenon of supersonic combustion in the staged-strut scramjet engine S Zhu, X Xu, Q Yang, Y Jin Aerospace Science and Technology 79, 70-74, 2018 | 51 | 2018 |
| Flame stabilization and propagation in dual-mode scramjet with staged-strut injectors S Zhu, X Xu, P Ji AIAA Journal 55 (1), 171-179, 2017 | 37 | 2017 |
| Hysteresis of mode transition in a dual-struts based scramjet Z Yan, Z Shaohua, C Bing, X Xu Acta Astronautica 128, 147-159, 2016 | 37 | 2016 |
| Numerical investigation of flame appearance and heat flux and in a deep-throttling variable thrust rocket engine Y Jin, X Xu, Q Yang, S Zhu Aerospace Science and Technology 88, 457-467, 2019 | 28 | 2019 |
| Experimental study on flame transition in a two-stage struts dual-mode scramjet SH Zhu, X Xu Journal of Aerospace Engineering 30 (5), 06017002, 2017 | 20 | 2017 |
| Experimental detection of two-dimensional temperature distribution in rocket-based combined cycle combustion chamber using multispectral imaging processing S Zheng, W Cai, B Liu, S Zhu, B Zhou, R Sui, Q Lu Fuel 333, 126391, 2023 | 17 | 2023 |
| Application of the vortex effects induced by the trailing wedge to enhance the mixing and combustion in the strut-based scramjet S Zhu, X Xu, Q Yang Applied Thermal Engineering 140, 604-614, 2018 | 14 | 2018 |
| 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 |
| 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 |
| Numerical study on the dynamic process of ramjet/scramjet mode transition in the integrated full flow path for RBCC engine YS Liu, R Xue, JL Liu, CQ Xu, SH Zhu, B Liu Applied Thermal Engineering 231, 121017, 2023 | 6 | 2023 |
| Effect of second-stage configuration on combustion in a dual-struts based staged supersonic combustor L Tian, Z Shaohua, Z Qin, L Xuan, X Xu 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 3780, 2014 | 6 | 2014 |
| Experimental study on ignition and blowout characteristics of dual combined flame stabilizers in scramjet F Qin, X Chen, S Zhu, B Liu, J Zhang, Y Gao, L Tan Aerospace Science and Technology 142, 108634, 2023 | 5 | 2023 |
| Numerical study on the dynamic process of ramjet/scramjet mode transition in the integrated RBCC full flow path through multistage fuel injection strategies YS Liu, R Xue, JL Liu, CQ Xu, SH Zhu, B Liu International Communications in Heat and Mass Transfer 146, 106857, 2023 | 5 | 2023 |
| Investigation on geometric throat matching characteristics of variable geometry rocket-based combined cycle combustor S Nie, J Ye, X Wei, F Qin, S Zhu, Y Wang, G He Acta Astronautica 209, 104-116, 2023 | 4 | 2023 |
| The preliminary study of oxygen-centered kerosene-swirl coaxial injector L Xuan, L Tian, H Jinli, Z Shaohua, X Xu 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 3587, 2014 | 4 | 2014 |
| Experimental investigations of a GO2/kerosene ejector rocket chamber for the RBCC propulsion system S Zhu, L Tian, L Xuan, X Xu 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 3989, 2014 | 4 | 2014 |
| The Confirmation of Thermal Boundary Parameters in an Oxygen Kerosene Fuel-Rich Rocket Engine X Wei, Z Yang, S Zhu, Z Zhao, J Ye, OJ Haidn Aerospace 9 (7), 343, 2022 | 3 | 2022 |
| Combustion performance investigation of a dual-struts scramjet P JI, X XU, B CHEN, S ZHU, G LIU 北京航空航天大学学报 43 (2), 366-374, 2017 | 3 | 2017 |
| Numerical investigation of the effect of reaction models on the supersonic combustion of liquid kerosene L Gang, ZS Hua, T Liang, L Yu, X Xu 51st AIAA/SAE/ASEE Joint Propulsion Conference, 4167, 2015 | 3 | 2015 |
| Numerical simulation on flow and heat transfer characteristics of film/regenerative compound cooling process J Xu, T Jing, Y Li, F Qin, S Zhu 2021 12th International Conference on Mechanical and Aerospace Engineering …, 2021 | 2 | 2021 |
