关注
Shaowen CHEN 陈绍文
Shaowen CHEN 陈绍文
哈尔滨工业大学教授
在 hit.edu.cn 的电子邮件经过验证
标题
引用次数
引用次数
年份
Effect of pleat shape on reverse pulsed-jet cleaning of filter cartridges
S Chen, Q Wang, DR Chen
Powder Technology 305, 1-11, 2017
562017
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
482018
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
342010
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
312018
Annular-slit nozzles for reverse flow cleaning of pleated filter cartridges
S Chen, DR Chen
Separation and Purification Technology 177, 182-191, 2017
312017
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
282019
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
272019
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
272013
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
262020
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
252013
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
242010
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
222020
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
222019
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
222018
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
212018
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
202013
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
192016
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
172023
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
172020
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
162021
系统目前无法执行此操作,请稍后再试。
文章 1–20