Numerical investigation of stator suction-type self-circulating casing treatment effects on the aerodynamic performance of a single-stage axial flow compressor

This study addresses the technical challenge that conventional self-recirculating casing treatments predominantly enhance the compressor stability with minimal efficiency gains. Focusing on a transonic axial flow compressor, National Aeronautics and Space Administration Stage35, the research designe...

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Veröffentlicht in:	Physics of fluids (1994) 2024-11, Vol.36 (11)
Hauptverfasser:	Zhang, Haoguang, Wang, Hao, Xiao, Jinhang, Feng, Yiming, Chu, Wuli
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamic stability Aeronautics Boundary layer stability Circulation Compressor efficiency Efficiency Flow separation Low speed Rotors Stalling Stators Suction Transonic flow Turbocompressors
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