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Impact of Leakage Inlet Swirl Angle in a Rotor–Stator Cavity on Flow Pattern, Radial Pressure Distribution and Frictional Torque in a Wide Circumferential Reynolds Number Range
 
 
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Int. J. Turbomach. Propuls. Power 2020, 5(2), 8; https://doi.org/10.3390/ijtpp5020008
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