| An experimental study on CH4/O2 continuously rotating detonation wave in a hollow combustion chamber W Lin, J Zhou, S Liu, Z Lin Experimental Thermal and Fluid Science 62, 122-130, 2015 | 148 | 2015 |
| Experimental study on propagation mode of H2/Air continuously rotating detonation wave W Lin, J Zhou, S Liu, Z Lin, F Zhuang International Journal of Hydrogen Energy 40 (4), 1980-1993, 2015 | 144 | 2015 |
| Experimental realization of H2/air continuous rotating detonation in a cylindrical combustor SJ Liu, ZY Lin, WD Liu, W Lin, FC Zhuang Combustion Science and Technology 184 (9), 1302-1317, 2012 | 99 | 2012 |
| Experimental investigation on detonation combustion patterns of hydrogen/vitiated air within annular combustor C Wang, W Liu, S Liu, L Jiang, Z Lin Experimental Thermal and Fluid Science 66, 269-278, 2015 | 89 | 2015 |
| Numerical investigation of a rotating detonation engine under premixed/non-premixed conditions J Sun, J Zhou, S Liu, Z Lin Acta astronautica 152, 630-638, 2018 | 73 | 2018 |
| Experimental and three-dimensional numerical investigations on H2/air continuous rotating detonation wave SJ Liu, ZY Lin, WD Liu, W Lin, MB Sun Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2013 | 69 | 2013 |
| Effects of injection nozzle exit width on rotating detonation engine J Sun, J Zhou, S Liu, Z Lin, J Cai Acta Astronautica 140, 388-401, 2017 | 65 | 2017 |
| Experimental verification of air-breathing continuous rotating detonation fueled by hydrogen C Wang, W Liu, S Liu, L Jiang, Z Lin international journal of hydrogen energy 40 (30), 9530-9538, 2015 | 64 | 2015 |
| Adaptive mesh refinement based simulations of three-dimensional detonation combustion in supersonic combustible mixtures with a detailed reaction model X Cai, J Liang, R Deiterding, Y Che, Z Lin international journal of hydrogen energy 41 (4), 3222-3239, 2016 | 54 | 2016 |
| Plume flowfield and propulsive performance analysis of a rotating detonation engine J Sun, J Zhou, S Liu, Z Lin, W Lin Aerospace Science and Technology 81, 383-393, 2018 | 52 | 2018 |
| Numerical investigation of a non-premixed hollow rotating detonation engine J Sun, J Zhou, S Liu, Z Lin, W Lin international journal of hydrogen energy 44 (31), 17084-17094, 2019 | 47 | 2019 |
| Thrust vectoring of a continuous rotating detonation engine by changing the local injection pressure SJ Liu, ZY Lin, MB Sun, WD Liu Chinese Physics Letters 28 (9), 094704, 2011 | 46 | 2011 |
| Effects of air injection throat width on a non-premixed rotating detonation engine J Sun, J Zhou, S Liu, Z Lin, W Lin Acta Astronautica 159, 189-198, 2019 | 44 | 2019 |
| Experimental research on the propagation characteristics of continuous rotating detonation wave near the operating boundary S Liu, W Liu, Z Lin, W Lin Combustion Science and Technology 187 (11), 1790-1804, 2015 | 44 | 2015 |
| Free jet test of continuous rotating detonation ramjet engine S Liu, W Liu, Y Wang, Z Lin 21st AIAA International Space Planes and Hypersonics Technologies Conference …, 2017 | 41 | 2017 |
| Parametric study of detonation initiation using a hot jet in supersonic combustible mixtures X Cai, J Liang, Z Lin, R Deiterding, Y Liu Aerospace Science and Technology 39, 442-455, 2014 | 38 | 2014 |
| Numerical study on thermodynamic efficiency and stability of oblique detonation waves S Miao, J Zhou, Z Lin, X Cai, S Liu AIAA Journal 56 (8), 3112-3122, 2018 | 37 | 2018 |
| Experimental investigations of detonation initiation by hot jets in supersonic premixed flows X Han, J Zhou, ZY Lin Chinese Physics B 21 (12), 124702, 2012 | 37 | 2012 |
| Adaptive mesh refinement–based numerical simulation of detonation initiation in supersonic combustible mixtures using a hot jet X Cai, J Liang, Z Lin, R Deiterding, H Qin, X Han Journal of Aerospace Engineering 28 (1), 04014046, 2015 | 28 | 2015 |
| Effects of dynamic backpressure on shock train motions in straight isolator J Cai, J Zhou, S Liu, Z Lin Acta Astronautica 141, 237-247, 2017 | 27 | 2017 |
