| Experimental research on the instability propagation characteristics of liquid kerosene rotating detonation wave Q Zheng, H Meng, C Weng, Y Wu, W Feng, M Wu Defence Technology 16 (6), 1106-1115, 2020 | 66 | 2020 |
| Influence of equivalence ratio on the propagation characteristics of rotating detonation wave B Li, Y Wu, C Weng, Q Zheng, W Wei Experimental thermal and fluid science 93, 366-378, 2018 | 65 | 2018 |
| Numerical research on kerosene/air rotating detonation engines under different injection total temperatures F Wang, C Weng, Y Wu, Q Bai, Q Zheng, H Xu Aerospace Science and Technology 103, 105899, 2020 | 51 | 2020 |
| An experimental study on the detonation transmission behaviours in acetylene-oxygen-argon mixtures Y Wu, Q Zheng, C Weng Energy 143, 554-561, 2018 | 50 | 2018 |
| Experimental research on the performance of a rotating detonation combustor with a turbine guide vane Y Wu, C Weng, Q Zheng, W Wei, Q Bai Energy 218, 119580, 2021 | 44 | 2021 |
| Propagation mode analysis of rotating detonation waves fueled by liquid kerosene H Meng, Q Zheng, C Weng, Y Wu, W Feng, G Xu, F Wang Acta Astronautica 187, 248-258, 2021 | 41 | 2021 |
| Stability of spinning detonation waves Y Wu, JHS Lee Combustion and Flame 162 (6), 2660-2669, 2015 | 33 | 2015 |
| Characterization of wave modes in a kerosene-fueled rotating detonation combustor with varied injection area ratios G Xu, Y Wu, Q Xiao, C Ding, Y Xia, Q Li, C Weng Applied Thermal Engineering 212, 118607, 2022 | 27 | 2022 |
| Effects of the oxygen mass fraction on the wave propagation modes in a kerosene-fueled rotating detonation combustor C Ding, Y Wu, G Xu, Y Xia, Q Li, C Weng Acta Astronautica 195, 204-214, 2022 | 27 | 2022 |
| Effects of total pressures and equivalence ratios on kerosene/air rotating detonation engines using a paralleling CE/SE method F Wang, C Weng, Y Wu, Q Bai, Q Zheng, H Xu Defence Technology 17 (6), 1805-1816, 2021 | 25 | 2021 |
| Influence of propagation direction on operation performance of rotating detonation combustor with turbine guide vane W Wei, Y Wu, C Weng, Q Zheng Defence Technology 17 (5), 1617-1624, 2021 | 21 | 2021 |
| On the wave propagation modes and operation range in rotating detonation combustor with varied injection and outlet throat Y Wu, G Xu, C Ding, C Weng Physics of Fluids 35 (1), 2023 | 16 | 2023 |
| Effects of an acoustic atomizer upon liquid-fueled detonation initiations in a detonation tube Y Wu, Q Han, G Yang Experimental Thermal and Fluid Science 109, 109863, 2019 | 13 | 2019 |
| Experimental study on propagation, quenching, and re-initiation characteristics of rotating detonation wave with liquid kerosene–oxygen-enriched air X Han, Y Wang, Q Zheng, Y Huang, Q Xiao, H Xu, Y Wu, W Feng, C Weng Experimental Thermal and Fluid Science 148, 110984, 2023 | 7 | 2023 |
| Study of the characteristics and combustion efficiency of liquid kerosene/oxygen-enriched air rotating detonation wave with different modes X Han, Y Huang, Q Zheng, Q Xiao, H Xu, F Wang, Y Wu, W Feng, C Weng Fuel 355, 129424, 2024 | 4 | 2024 |
| Wave mode analysis of a turbine guide vane-integrated rotating detonation combustor based on instantaneous frequency identification C Ding, Y Wu, Y Huang, Q Zheng, Q Li, G Xu, C Kang, C Weng Energy 284, 128612, 2023 | 4 | 2023 |
| Numerical investigation on the interactions between rotating detonation wave complex and planar turbine cascade Q Li, Y Wu, Y Xia, X Li, C Weng Energy Science & Engineering 11 (1), 410-429, 2023 | 4 | 2023 |
| Propagation behaviors of kerosene-fueled rotating detonation wave with varied atomizer locations G Xu, Y Wu, C Kang, T Lei, Y Qiu, C Ding, C Weng Aerospace Science and Technology 142, 108676, 2023 | 3 | 2023 |
| Combustion characteristics of rotating detonation based on liquid hydrocarbon fuel D Chenwei, W Chunsheng, W Yuwen, BAI Qiaodong, W Xiaowei, ... 爆炸与冲击 42 (2), 022101-1-022101-16, 2022 | 3 | 2022 |
| Three-Dimensional Numerical Simulation of H2/Air Continuous Rotating Detonation Flow Field Based on OpenFOAM M Hao-long, W Chun-sheng, WU Yu-wen, Z Quan, WEI Wan-li Journal of Propulsion Technology 41 (6), 1351, 2020 | 2 | 2020 |
