Study of the optimal location of wing sensors using model-order reduction
Document typeBachelor thesis
Rights accessOpen Access
The overall goal of this work is to numerically determine the optimal location of sensors for predicting the vibration behavior of a wing. The methodology to achieve this goal will be to construct, using as starting point finite element simulations, a reduced-order model able to capture the essential vibrational characteristic of the wing.
SubjectsAirplanes--Wings, Vibration (Aeronautics), Finite element method, Avions -- Ales, Vibració (Aeronàutica), Elements finits, Mètode dels
DegreeGRAU EN ENGINYERIA EN TECNOLOGIES AEROESPACIALS (Pla 2010)