Integrated Structural Design and Vibration Suppression Using Independent Modal Space Control
Methodology for implementing fracture mechanics in global structural design of aircraft
Aeroelastic Shape Optimization of a Flapping Wing (AIAA 2014-0469)
Continuum Shape Sensitivity with Spatial Gradient Reconstruction of Built-up Structures
Reliability analysis of a large computational model using polynomial chaos expansion
Nonlinear Aeroelastic Scaled Model Optimization Using Equivalent Static Loads
Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects
Methodology for Implementing Fracture Mechanics in Global Structural Design of Aircraft
Design and Evaluation of Aeroelastically Tuned Joined-Wing SensorCraft Flight Test Article