-Approach validated for fixed wing.
-Aeroelasticity of a Launch Vehicles
- Aeroelasticity of a maneuvering vehicle using a F.E. based description
- Perturbation methods and Normal Form analysis
- Analytical and Computational Aeroelasticity
- First-principle based, Time- and Frequency-domain descriptions of viscoelasticity.
- Viscoelasticity v.s. modal analysis
- Multi-Objective-Optimization (M.O.O.) v.s. Single-Objective-Optimization
- The challenge of unconventional optimization problem.