ASCENT TRAJECTORY OPTIMIZATION OF HYPERSONIC VEHICLE USING SWARM INTELLIGENT METHOD
A POD-based Reduced Order Design Scheme for Shape Optimization of Air Vehicles
Extension of MSC Nastran UVLM.OpenFSI for Rotational Applications Including Wind Turbines
Dynamic Nonlinear Aeroelastic Analysis of the Joined Wing Configuration
Continuous Dynamic Simulation for Morphing Wing Aeroelasticity
Enabling Sensitivity Analysis Capability for a CFD-Based Unsteady Aerodynamic/Aeroelastic Solver
AIAA-2006-1640 Time Domain Nonlinear Aeroelastic Analysis for HALE Wings
A HYBRID OPTIMIZATION STRATEGY USING DESIGN-SPACE EVOLUTION AND POD-BASED ORDER REDUCTION