Numerical investigation of the first stall stage in a counter-rotating axial-flow compressor with large tip clearance and speed ratio effects under casing treatment
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Published online on February 14, 2026
Abstract
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Ahead of Print.
Single-passage steady-state numerical simulations were used to study the first stall stage of a counter-rotating axial-flow compressor (CRAC) under a large tip clearance of 1 mm and rotating speed ratio effects. The first stall stage is evaluated by ...
Single-passage steady-state numerical simulations were used to study the first stall stage of a counter-rotating axial-flow compressor (CRAC) under a large tip clearance of 1 mm and rotating speed ratio effects. The first stall stage is evaluated by ...