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Numerical investigations of circumferential nonuniformity and model refinement under inlet distortion effects

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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.
The inlet distortion issue in propulsion systems leads to a degradation of compressor performance and induces aerodynamic instability. To assess the impact of total pressure distortion on performance and stability, a parallel compressor modeling study and ...