Establish a Finite Element model of the Hub with shafts, bearings and gears
Calculate Hub global and local stresses and accelerations based on unit aerodynamic loads
Identify maximum stress concentration factor areas
Based on Finite Element results, identify sensor positions
Establish Strain gauge and/or accelerometer positions and directions
Start monitoring
Correlate Finite Element results with monitoring results
Link results to the CAE Fatigue software
Calculate remaining fatigue life
Pre-project to monitor a simple loading process
Monitoring shafts, bearing and gears