PDF
…Aeroelastic consequences:
Linear: flutter, dynamic loads
Nonlinear: buckling / flutter interactions, limit cycle oscillations, vibrations
Worst case scenarios
Reliability
Design and maintenance practices
University of Washington
4
Some sources of uncertainty in composite structures
Damage
Delamination
Joint/attachment changes
Debonding…
https://www.wichita.edu/industry_and_defense/NIAR/Documents/300_Tuesday_Livne.pdf