tailieuchung - Effect of recirculation channel on aerodynamic performance of a single-stage transonic axial compressor

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Effect of recirculation channel on aerodynamic performance of a single-stage transonic axial compressor

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This paper investigates the effects of recirculation channel on the performance of a single-stage transonic axial compressor, NASA Stage 37, such as pressure ratio, adiabatic efficiency, and operating range. Numerical analysis was conducted by solving three-dimensional steady Reynolds-averaged Navier-Stokes equations with the k-epsilon turbulence model. |

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Effect of recirculation channel on aerodynamic performance of a single-stage transonic axial compressor

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