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Numerical investigation on discrete circumferential grooves casing treatment of axial flow compressor

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Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Published online on

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 ...