1. Aeroengine design manual General editorial board. Aeroengine design manual volume ten: Turbine. Aviation Industry Press, Beijing (2001)
2. Lepicovsky, J.: Effects of a Rotating Aerodynamic Probe on the Flow Field of a Compressor Rotor. NASA/CR-2008–215215
3. Coldrick, S., Ivey, P., Wells, R.: Considerations for using 3-D pneumatic probes in high-speed axial rotor compressors. J. Turbomach. 125, 149–154 (2003)
4. Shaohui, L.I.: Influence of probe support rod on compressor downstream flow field. Beijing University of Aeronautics and Astronautics, Beijing (2013)
5. Yang, R., Zhao, J., Xiang, H., et al.: Effects of inlet probe support on aerodynamic performance of 1.5-stage compressor. J. Propul. Technol. 38(5), 1038–1046 (2017)