Effect of pleat shape on reverse pulsed-jet cleaning of filter cartridges S Chen, Q Wang, DR Chen Powder Technology 305, 1-11, 2017 | 56 | 2017 |
Flow separation control using unsteady pulsed suction through endwall bleeding holes in a highly loaded compressor cascade H Zhang, S Chen, Q Meng, S Wang Aerospace Science and Technology 72, 455-464, 2018 | 48 | 2018 |
Effects of boundary layer suction on aerodynamic performance in a high-load compressor cascade G Shuang, C Shaowen, S Yanping, S Yufei, C Fu Chinese Journal of Aeronautics 23 (2), 179-186, 2010 | 34 | 2010 |
Effect of axisymmetric endwall contouring on the high-load low-reaction transonic compressor rotor with a substantial meridian contraction S Sun, S Chen, W Liu, Y Gong, S Wang Aerospace Science and Technology 81, 78-87, 2018 | 31 | 2018 |
Annular-slit nozzles for reverse flow cleaning of pleated filter cartridges S Chen, DR Chen Separation and Purification Technology 177, 182-191, 2017 | 31 | 2017 |
Treatment and optimization of casing and blade tip for aerodynamic control of tip leakage flow in a turbine cascade S Jiang, F Chen, J Yu, S Chen, Y Song Aerospace Science and Technology 86, 704-713, 2019 | 28 | 2019 |
The impact of various forward sweep angles on the performance of an ultra-high-load low-reaction transonic compressor rotor S Sun, S Wang, S Chen, C Tao, L Cai, J Chen Applied Thermal Engineering 150, 953-966, 2019 | 27 | 2019 |
Control of flow separations in compressor cascade by boundary layer suction holes in suction surface J Ding, S Chen, H Xu, S Sun, S Wang Turbo Expo: Power for Land, Sea, and Air 55225, V06AT35A012, 2013 | 27 | 2013 |
Performance optimization of a krypton Hall thruster with a rotating propellant supply G Xia, H Li, Y Ding, L Wei, S Chen, D Yu Acta Astronautica 171, 290-299, 2020 | 26 | 2020 |
Influence of local surface roughness of rotor blade on performance of an axial compressor stage S Chen, S Sun, H Xu, L Zhang, S Wang, T Zhang Turbo Expo: Power for Land, Sea, and Air 55225, V06AT35A015, 2013 | 25 | 2013 |
Enhancing aerodynamic performances of a high-turning compressor cascade via boundary layer suction S Guo, SW Chen, HW Lu, YP Song, F Chen Science China Technological Sciences 53, 2748-2755, 2010 | 24 | 2010 |
Design, modification and optimization of an ultra-high-load transonic low-reaction aspirated compressor S Sun, S Wang, S Chen Aerospace Science and Technology 105, 105975, 2020 | 22 | 2020 |
Thermal performance of blade tip and casing coolant injection on a turbine blade with cavity and winglet-cavity tip Z Zhou, S Chen, W Li, S Wang International Journal of Heat and Mass Transfer 130, 585-602, 2019 | 22 | 2019 |
Aerodynamic optimisation of a winglet-cavity tip in a high-pressure axial turbine cascade Z Zhou, S Chen, S Wang Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2018 | 22 | 2018 |
Experiment study of aerodynamic performance for the suction-side and pressure-side winglet-cavity tips in a turbine blade cascade Z Zhou, S Chen, W Li, S Wang, X Zhou Experimental Thermal and Fluid Science 90, 220-230, 2018 | 21 | 2018 |
Experimental study of the impact of hole-type suction on the flow characteristics in a high-load compressor cascade with a clearance SW Chen, SJ Sun, H Xu, ST Wang Experimental thermal and fluid science 51, 220-226, 2013 | 20 | 2013 |
Numerical study of reverse multi-pulsing jet cleaning for pleated cartridge filters S Chen, DR Chen Aerosol and Air Quality Research 16 (8), 1991-2002, 2016 | 19 | 2016 |
Flow instability control of an ultra-highly loaded transonic compressor rotor using self-excited casing bleed S Ding, S Chen, S Hao, S Wang Physics of Fluids 35 (6), 2023 | 17 | 2023 |
The influence of diversified forward sweep heights on operating range and performance of an ultra-high-load low-reaction transonic compressor rotor S Sun, S Wang, S Chen Energy 194, 116857, 2020 | 17 | 2020 |
Numerical study of dual sweeping jet actuators for corner separation control in compressor cascade Q Meng, X Du, S Chen, S Wang Journal of Thermal Science 30, 201-209, 2021 | 16 | 2021 |