Effects of Rotor-Bleeding Airflow on Aerodynamic and Structural Performances of a Single-Stage Transonic Axial Compressor
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DOI: 10.1007/s42405-019-00239-5
Abstract: This paper presents the effects of airflow bleed from the rotor shroud surface between leading and trailing edges on aerodynamic and structural performances of a single-stage transonic axial compressor, NASA stage 37, using three-dimensional Reynolds-averaged… read more here.
Keywords: transonic axial; rotor; aerodynamic structural; axial compressor ... See more keywords