FE-based reduced order models for rotordynamic and aeroelastic analysis of aircraft engines (Master Thesis, UniPD)
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Updated
May 15, 2026 - MATLAB
FE-based reduced order models for rotordynamic and aeroelastic analysis of aircraft engines (Master Thesis, UniPD)
This project develops a physics-based simulator for the Jeffcott (Laval) rotor model of a flexible rotating shaft that generates vibration signals under different fault conditions. This serves as a tool for studying fault signatures and developing diagnostic algorithms.
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