Numerical investigation and modeling of sweep effects on inlet flow field of axial compressor cascades

A spanwise loss model for axial compressor stator based on machine learning

(2022) Zixuan YUE et al.   Chinese Journal of Aeronautics

Development of a Throughflow-Based Simulation Tool for Preliminary Compressor Design Considering Blade Geometry in Gas Turbine Engine

(2021) Xiaoheng Liu et al.   Applied Sciences-Basel

Investigation and Verification of the Aerodynamic Performance of a Fan/Booster with Through-flow Method

(2018) Xiaoheng Liu et al.   Journal of Thermal Science

Modeling and numerical investigation of the inlet circumferential fluctuations of swept and bowed blades

(2017) Mingzhi Tang et al.   Journal of Thermal Science

Investigation of non-axisymmetric endwall contouring in a compressor cascade

(2017) Xiwu Liu et al.   Journal of Thermal Science

Effect of blade sweep on inlet flow in axial compressor cascades

(2015) Hao Chang et al.   Chinese Journal of Aeronautics

Effects of inlet circumferential fluctuation on the sweep aerodynamic performance of axial fans/compressors

(2013) Xingmin Gui et al.   Journal of Thermal Science