Numerical investigation on discrete circumferential grooves casing treatment of axial flow compressor
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Published online on May 07, 2026
Abstract
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Ahead of Print.
To ensure that aeroengines could adapt to complex operating conditions, stability margin is one of the mandatory indicators in the design process of axial-flow compressors. Expanding the stable operating range of compressors using flow control ...
To ensure that aeroengines could adapt to complex operating conditions, stability margin is one of the mandatory indicators in the design process of axial-flow compressors. Expanding the stable operating range of compressors using flow control ...