Document is current

Any future updates will be listed below

Modeling and Prediction of Erosion Rate for Aero-Engine Compressor Blades Using an Integrated Framework Based on Improved Harris Hawks Optimization with XGBoost and SHAP

Crossref DOI link: https://doi.org/10.1007/s11668-025-02306-4

Published Online: 2025-10-15

Published Print: 2025-12

Update policy: https://doi.org/10.1007/springer_crossmark_policy

About CrossMark