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.
Wave propagation and band gap analysis of longitudinally periodic rotors, in Python.
Vibration and rotor dynamics library, SDOF to FE shaft with Campbell diagrams, every model tested against closed form results
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