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Effect of blade squealer tips on aerodynamic performance and stall margin in a transonic centrifugal compressor with vaned diffuser

Transonic Centrifugal CompressorEngineeringAerospace EngineeringFluid MechanicsMechanical EngineeringCompressorBlade Squealer TipsAerodynamicsAerodynamic PerformancePropulsionGas Turbine EngineFluid Machinery