System identification of the simulated in-flight loads

Modified intertially coupled equqtions of motion for a flexible aircraft with coupled vibrations

Aeroelastic loads modeling for composite aircraft design support

Effects of Flexibility on Aircraft Dynamic Loads and Structural Optimization

Modified Inertially Coupled Equqtions of Motion for a Flexible Aircraft with Bending-Torsion Coupled Beams

Dynamic Loads Optimizaiton during Atmospheric turbulence on a Flexible Aircraft