AIAA-2001-1459 Volterra Series Approach for Nonlinear Aeroelastic Response of 2-D Lifting Surfaces
AIAA-2001-1213 Development of Unsteady Aerodynamic State-Space Models from CFD-Based Pulse Responses
Core and Face Sheet Anisotropy in Deformation and Buckling of Sandwich Panels
Flutter Characterization of the Flexible HSCT Semispan Model
Aeroelastic System Development Using Proper Orthogonal Decomposition and Volterra Theory
Analysis of a 2-D Supersonic Lifting Surface with Time Delayed Feedback Control
Thin-Walled Rotating Blades made of Functionally Graded Materials: Modeling and Vibration Analysis