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This document discusses a new method called the Advanced Recontouring Process (ARP) for recontouring the leading edges of worn jet engine compressor blades. The ARP aims to define optimized new leading edge geometries through numerical flow simulations to improve aerodynamic performance. Worn blades were classified into 9 categories based on measurements. Flow simulations were performed on the original and worn profiles to analyze the effects of erosion. The ARP seeks to standardize the recontouring process

Author

inam vf

Language

EN