轴向超音通流风扇流动机理
[1] Sun S*, Li X, Guo M, Song J, Yang C, Wang J. Effect of inlet Mach number on performance and flow structure of an axial supersonic through-flow fan cascade[J]. Physics of Fluids, 2023. 35(5): 056104.
[2] 孙士珺*, 李晓龙, 刘艳明, 王建华, 王松涛. 宽速域来流对超音通流风扇叶型气动性能的影响[J]. 航空学报, 2023, 44(21): 528523.
[3] Sun S*, Zhou L, Ji L. Influence of Solidity on Aerodynamic Performance of Axial Supersonic Through-Flow Fan Cascades[J]. AIAA Journal of Propulsion and Power, 2022: 1-14.
[4] Sun S*, Hao J, Yang J, et al. Impacts of tandem configurations on the aerodynamic performance of an axial supersonic through-flow fan cascade[J]. ASME Journal of Turbomachinery, 2021: 1-25.
[5] 轴向超声速通流串列构型弦长比对气动性能影响的数值研究[J]. 推进技术, 2021.
高负荷风扇/压气机气动设计
[6] Sun S*, Wang S, Zhang L, et al. Design and performance analysis of a two-stage transonic low-reaction counter-rotating aspirated fan/compressor with inlet counter-swirl [J]. Aerospace Science and Technology, 2021, 111: 106519.
[7] Sun S*, Wang S, Chen S. Design, modification and optimization of an ultra-high-load transonic low-reaction aspirated compressor [J]. Aerospace Science and Technology, 2020, 105: 105975.
[8] 孙士珺*, 王松涛, 陈绍文, 胡应交, 张龙新. 高负荷低反力度吸附式风扇气动设计与性能分析[J]. 推进技术, 2018; 39(3):547-555.
[9] Sun S*, Wang S, Chen S. Aerodynamic design and analysis of a two-stage high-load low-reaction transonic aspirated counter-rotating compressor [C]. ASME Paper GT2017-64144, 2017.
主、被动流动控制技术（附面层抽吸、弯掠三维造型等）
[10] Sun S*, Wang S, Chen S. The influence of diversified forward sweep heights on operating range and performance of an ultra-high-load low-reaction transonic compressor rotor [J]. Energy, 2020, 194: 116857.
[11] Sun S*, Wang S, Chen S*, et al. The impact of various forward sweep angles on the performance of an ultra-high-load low-reaction transonic compressor rotor [J]. Applied Thermal Engineering, 2019, 150: 953-966.
[12] Sun S*, Chen S*, Liu W, et al. Effect of axisymmetric endwall contouring on the high-load low-reaction transonic compressor rotor with a substantial meridian contraction [J]. Aerospace Science and Technology, 2018, 81: 78-87.
[13] 孙士珺*, 陈绍文, 刘维, 王松涛. 轮缘曲线对低反力度跨音速高负荷转子性能影响的数值研究[J]. 推进技术, 2018; 39(12):2710-2717.
[14] Chen S*, Sun S, Lan Y, Wang S. The effect of different clearance geometry configurations on aerodynamic performance in a high-load compressor cascade [J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2014, 228(8): 1425-1433.
[15] 孙士珺, 陈绍文*, 王春雪, 王松涛. 孔式抽吸对带间隙高负荷压气机性能的影响. 推进技术, 2014; 35(9):1202-1208.
[16] 陈绍文*, 孙士珺, 兰云鹤, 周治华, 王松涛. 来流附面层对吸附式压气机叶栅影响的数值研究. 机械工程学报, 2014; 50(24):158-163.
[17] 陈绍文*, 孙士珺, 韩东, 徐皓, 王松涛. 间隙大小对高负荷压气机叶栅流动特性的影响. 工程热物理学报, 2014; 35(1):34-37.
[18] Chen S*, Sun S, Xu H, Wang S. Experimental study of the impact of hole-type suction on the flow characteristics in a high-load compressor cascade with a clearance [J]. Experimental thermal and fluid science, 2013, 51: 220-226.
[19] 孙士珺, 陈绍文*, 韩东, 徐皓, 王松涛. 附面层吸除对带间隙的高负荷压气机叶栅流动特性影响的实验研究. 工程热物理学报, 2013; 34(9):1645-1648.
风扇/压气机污垢沉积
[20] Chen S*, Xu H, Sun S, et al. Influence of Additional Leading-Edge Surface Roughness on Performances in Highly Loaded Compressor Cascade [J]. International Journal of Turbo & Jet-Engines, 2015, 32(2): 155-163.
[21] Chen S*, Sun S, Xu H, Zhang L, Wang S, Zhang T. Influence of local surface roughness of rotor blade on performance of an axial compressor stage [C]. ASME Paper GT2013- 94816, 2013.
代表性专利：
[1] 孙士珺, 刘艳明. 一种轴向超音通流风扇串列构型及串列构型优化方法，2023-2-3, 中国，202111522842.X.
[2] 孙士珺, 刘艳明. 一种基于轴向超音来流变几何风扇的宽速域冲压发动机，2023-2-3, 中国，202210005349.9.
[3] 孙士珺, 李晓龙, 张英刚, 王骥翔, 黄叶红, 马奕然, 李心唱. 一种航空涡扇发动机用变形风扇及优化方法, 2023-7-7, 中国，202310063107.X.
[4] 陈绍文，孙士珺，巩赟，王松涛. 压气机的静叶与端壁间的间隙流动控制方法及压气机，2018-04-06，中国，ZL201610986341.X.
