轴向超音通流风扇
[1] 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]. Journal of Turbomachinery, 2021: 1-25.
[2] 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.(accepted).
高负荷风扇/压气机气动设计
高负荷风扇/压气机设计
[3] Sun S*, Wang S, Zhang L, Ji L. 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.
[4] Sun S*, Wang S, Chen S. Design, modification and optimization of an ultra-high-load transonic lowreaction aspirated compressor [J]. Aerospace Science and Technology, 2020, 105: 105975.
[5] 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.
[6] 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）
[7] 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.
[8] 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.
[9] 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.
[10] 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.
[11] 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.
[12] 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.
[13] 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.
[14] 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.
[15] 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.
[16] 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
[17] 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.
[18] 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] 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.
