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Study on the effect of leading edge erosion evolution on flow characteristics of subsonic and supersonic airfoils

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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 evolution of aviation engine fan blade leading-edge erosion characteristics with operating time was studied. Identifying the evolutionary features of the eroded leading edges facilitates the investigation of their impact on aerodynamic performance ...