| Modeling of spray jet flame under MILD condition with non-adiabatic FGM and a new conditional droplet injection model L Ma, D Roekaerts Combustion and Flame 165, 402-423, 2016 | 82 | 2016 |
| Numerical study of the multi-flame structure in spray combustion L Ma, D Roekaerts Proceedings of the Combustion Institute 36 (2), 2603-2613, 2017 | 59 | 2017 |
| Transported PDF modeling of ethanol spray in hot-diluted coflow flame L Ma, B Naud, D Roekaerts Flow, Turbulence and Combustion 96, 469-502, 2016 | 55 | 2016 |
| Ignition and combustion of a single aluminum particle in hot gas flow Y Feng, Z Xia, L Huang, L Ma Combustion and Flame 196, 35-44, 2018 | 54 | 2018 |
| Exprimental study on the evaporation characteristics of the kerosene gel droplet D Yang, Z Xia, L Huang, L Ma, Y Feng, Y Xiao Experimental Thermal and Fluid Science 93, 171-177, 2018 | 37 | 2018 |
| Ignition and combustion characteristics of single gas-atomized Al–Mg alloy particles in oxidizing gas flow Y Feng, L Ma, Z Xia, L Huang, D Yang Energy 196, 117036, 2020 | 36 | 2020 |
| Structure of spray in hot-diluted coflow flames under different coflow conditions: A numerical study L Ma, D Roekaerts Combustion and Flame 172, 20-37, 2016 | 35 | 2016 |
| Effect of ambient temperature on the ignition and combustion process of single aluminium particles Y Feng, Z Xia, L Huang, L Ma Energy 162, 618-629, 2018 | 34 | 2018 |
| Effects of turbulence-chemistry interactions on auto-ignition and flame structure for n-dodecane spray combustion Y Zhang, H Wang, A Both, L Ma, M Yao Combustion Theory and Modelling 23 (5), 907-934, 2019 | 31 | 2019 |
| Research progress on solid-fueled Scramjet Z Xiang, XIA Zhixun, MA Likun, LI Chaolong, F Chuanbo, B Natan, G Alon Chinese Journal of Aeronautics 35 (1), 398-415, 2022 | 30 | 2022 |
| Characteristics of the combustion chamber of a boron-based solid propellant ducted rocket with a chin-type inlet B Chen, Z Xia, L Huang, L Ma Aerospace Science and Technology 82, 210-219, 2018 | 30 | 2018 |
| Numerical study on solid-fuel scramjet combustor with fuel-rich hot gas X Zhao, Z Xia, B Liu, Z Lv, L Ma Aerospace Science and Technology 77, 25-33, 2018 | 26 | 2018 |
| Experimental and numerical study of solid rocket scramjet combustor equipped with combined cavity and strut device C Li, Z Xia, L Ma, X Zhao, B Chen Acta Astronautica 162, 145-154, 2019 | 25 | 2019 |
| Thermal decomposition and kinetics of electrically controlled solid propellant through thermogravimetric analysis Z He, Z Xia, J Hu, L Ma, Y Li Journal of Thermal Analysis and Calorimetry 139, 2187-2195, 2020 | 24 | 2020 |
| Influence of the vortex generator on the performance of solid rocket scramjet combustor C Li, X Zhao, Z Xia, L Ma, B Chen Acta Astronautica 164, 174-183, 2019 | 22 | 2019 |
| Experimental investigation of the effects of chamber length and boron content on boron-based gel fuel ramjet performance Y Xiao, Z Xia, L Huang, L Ma, D Yang Acta Astronautica 160, 101-105, 2019 | 22 | 2019 |
| Numerical investigation of ethanol spray-in-hot-coflow flame using steady flamelet model L Ma, S Zhu, M Tummers, T Van Der Meer, D Roekaerts Eighth Mediterranean Combustion Symposium, 1-12, 2013 | 22 | 2013 |
| Thermodynamic properties of polyvinyl alcohol binder of electrically controlled solid propellant Z He, Z Xia, J Hu, L Ma, Y Li Journal of Polymer Research 26, 1-8, 2019 | 21 | 2019 |
| Experimental study on aluminum particles combustion in a turbulent jet J Zhang, Z Xia, L Ma, L Huang, Y Feng, D Yang Energy 214, 118889, 2021 | 20 | 2021 |
| LES of the Sandia flame series DF using the Eulerian stochastic field method coupled with tabulated chemistry D Yifan, XIA Zhixun, MA Likun, LUO Zhenbing, X Huang, D Xiong Chinese Journal of Aeronautics 33 (1), 116-133, 2020 | 18 | 2020 |
