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A numerical study of the effect of the nose cone geometry on the performance of the centrifugal compressor in a micro-turbojet engine

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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.
Conventional research on compressor design often ignores the impact of the nose cone. This results in imprecise performance evaluations. By including the nose cone in the analysis, we can more accurately simulate operational conditions. This inclusion of ...