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Effect of tip clearance variation in the transonic axial compressor of a miniature gas turbine at different Reynolds numbers

EngineeringFluid MechanicsMechanical EngineeringCompressorGas Turbine CombustionTransonic Axial CompressorIn-cylinder FlowAerodynamicsFluid MachineryTip Clearance VariationGas Turbine EngineMiniature Gas Turbine