| Investigation of flame flashback phenomenon in a supersonic crossflow with ethylene injection upstream of cavity flameholder G Zhao, M Sun, J Wu, X Cui, H Wang Aerospace Science and Technology 87, 190-206, 2019 | 69 | 2019 |
| Suppression of combustion mode transitions in a hydrogen-fueled scramjet combustor by a multi-channel gliding arc plasma R Feng, J Zhu, Z Wang, F Zhang, Y Ban, G Zhao, Y Tian, C Wang, ... Combustion and Flame 237, 111843, 2022 | 47 | 2022 |
| On shock sensors for hybrid compact/WENO schemes GY Zhao, MB Sun, S Pirozzoli Computers & Fluids 199, 104439, 2020 | 42 | 2020 |
| A general framework for the evaluation of shock-capturing schemes G Zhao, M Sun, A Memmolo, S Pirozzoli Journal of Computational Physics 376, 924-936, 2019 | 38 | 2019 |
| Experimental investigations of cavity parameters leading to combustion oscillation in a supersonic crossflow GY Zhao, MB Sun, XL Song, XP Li, HB Wang Acta Astronautica 155, 255-263, 2019 | 25 | 2019 |
| Effects of injection on flame flashback in supersonic crossflow G Zhao, J Du, H Yang, T Tang, M Sun Aerospace Science and Technology 120, 107226, 2022 | 21 | 2022 |
| Investigation of combustion characteristics in a scramjet combustor using a modified flamelet model G Zhao, M Sun, H Wang, H Ouyang Acta Astronautica 148, 32-40, 2018 | 21 | 2018 |
| An efficient adaptive central-upwind WENO-CU6 numerical scheme with a new sensor GY Zhao, MB Sun, Y Mei, L Li, HB Wang, GX Li, Y Liu, YC Sun, CH Liang Journal of Scientific Computing 81, 649-670, 2019 | 20 | 2019 |
| Numerical dissipation control in an adaptive WCNS with a new smoothness indicator G Zhao, M Sun, S Xie, H Wang Applied Mathematics and Computation 330, 239-253, 2018 | 19 | 2018 |
| Numerical investigation of the scale effects of the flame flashback phenomenon in scramjet combustors G Zhao, J Du, M Liu, H Wang, M Sun Aerospace Science and Technology 119, 107165, 2021 | 17 | 2021 |
| Investigations of injection parameters on combustion oscillation in a supersonic crossflow GY Zhao, MB Sun, YN Wang, XP Li, HB Wang Acta Astronautica 152, 426-436, 2018 | 17 | 2018 |
| A conceptual design of shock-eliminating clover combustor for large scale scramjet engine M Sun, Y Zhao, G Zhao, Y Liu Acta Astronautica 130, 34-42, 2017 | 17 | 2017 |
| Effect of injection scheme on asymmetric phenomenon in rectangular and circular scramjets MA Guangwei, SUN Mingbo, Z Guoyan, C Liang, W Hongbo, YU Jiangfei Chinese Journal of Aeronautics 36 (1), 216-230, 2023 | 16 | 2023 |
| A flamelet model for supersonic non-premixed combustion with pressure variation GY Zhao, MB Sun, JS Wu, HB Wang Modern Physics Letters B 29 (21), 1550117, 2015 | 16 | 2015 |
| Effect of injection Mach number on penetration in a supersonic crossflow GX Li, MB Sun, JF Yu, CH Liang, Y Liu, GY Zhao, YH Huang AIAA Journal 58 (3), 1216-1226, 2020 | 14 | 2020 |
| An efficient low-dissipation hybrid central/WENO scheme for compressible flows L Li, HB Wang, GY Zhao, MB Sun, DP Xiong, T Tang International Journal of Computational Fluid Dynamics 34 (10), 705-730, 2020 | 13 | 2020 |
| Efficient WENOCU4 scheme with three different adaptive switches L Li, H Wang, G Zhao, M Sun, D Xiong, T Tang Journal of Zhejiang University-SCIENCE A 21 (9), 695-720, 2020 | 13 | 2020 |
| Numerical study of transverse jet mixing and combustion in a high-enthalpy supersonic crossflow with trace gases T Tang, Z Wang, J Yu, Y Huang, M Sun, H Wang, G Zhao, Y Yang, ... Physics of Fluids 35 (3), 2023 | 11 | 2023 |
| Evaluation of flamelet/progress variable model for the applications in supersonic combustion using hybrid RANS/LES approach T Tang, H Wang, M Sun, G Zhao, J Yu, Z Fan, Z Wang Aerospace Science and Technology 126, 107633, 2022 | 11 | 2022 |
| Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor M Liu, M Sun, G Zhao, Y Meng, Y Huang, G Ma, H Wang Aerospace Science and Technology 130, 107904, 2022 | 10 | 2022 |
Ming Bo SunNational University of Defense Technology, China在 nudt.edu.cn 的电子邮件经过验证
