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Journal: Applied SciencesVolume: 11Number: 3937
Article: Investigation of Seal Cavity Leakage Flow Effect on Multistage Axial Compressor Aerodynamic Performance with a Circumferentially Averaged Method
  • Authors:
  • Dong Liang1,
  • Donghai Jin1,2,* and
  • Xingmin Gui1,2
Link: https://www.mdpi.com/2076-3417/11/9/3937

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