軸向超音通流風扇流動機理
[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] 孫士珺*, 李曉龍, 劉豔明, 王建華, 王松濤. 寬速域來流對超音通流風扇葉型氣動性能的影響[J]. 航空學報, 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] 軸向超聲速通流串列構型弦長比對氣動性能影響的數值研究[J]. 推進技術, 2021.
高負荷風扇/壓氣機氣動設計
[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] 孫士珺*, 王松濤, 陳紹文, 胡應交, 張龍新. 高負荷低反力度吸附式風扇氣動設計與性能分析[J]. 推進技術, 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、被動流動控制技術（附面層抽吸、彎掠三維造型等）
[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] 孫士珺*, 陳紹文, 劉維, 王松濤. 輪緣曲線對低反力度跨音速高負荷轉子性能影響的數值研究[J]. 推進技術, 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] 孫士珺, 陳紹文*, 王春雪, 王松濤. 孔式抽吸對帶間隙高負荷壓氣機性能的影響. 推進技術, 2014; 35(9):1202-1208.
[16] 陳紹文*, 孫士珺, 蘭雲鶴, 周治華, 王松濤. 來流附面層對吸附式壓氣機葉栅影響的數值研究. 機械工程學報, 2014; 50(24):158-163.
[17] 陳紹文*, 孫士珺, 韓東, 徐皓, 王松濤. 間隙大小對高負荷壓氣機葉栅流動特性的影響. 工程熱物理學報, 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] 孫士珺, 陳紹文*, 韓東, 徐皓, 王松濤. 附面層吸除對帶間隙的高負荷壓氣機葉栅流動特性影響的實驗研究. 工程熱物理學報, 2013; 34(9):1645-1648.
風扇/壓氣機污垢沉積
[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.
代表性專利：
[1] 孫士珺, 劉豔明. 一種軸向超音通流風扇串列構型及串列構型優化方法，2023-2-3, 中國，202111522842.X.
[2] 孫士珺, 劉豔明. 一種基于軸向超音來流變幾何風扇的寬速域沖壓發動機，2023-2-3, 中國，202210005349.9.
[3] 孫士珺, 李曉龍, 張英剛, 王骥翔, 黃葉紅, 馬奕然, 李心唱. 一種航空渦扇發動機用變形風扇及優化方法, 2023-7-7, 中國，202310063107.X.
[4] 陳紹文，孫士珺，鞏赟，王松濤. 壓氣機的靜葉與端壁間的間隙流動控制方法及壓氣機，2018-04-06，中國，ZL201610986341.X.
