Advanced Telemedicine System Concepts for Planetary Exploration Missions
Aeroelastic optimization of high aspect ratio wings using an exact dynamic stiffness matrix method
Aeroelastic Optimization of High Aspect Ratio Wings Using an Exact Dynamic Stiffness Matrix Method
AEROELASTIC RESPONSE OF A FLEXEBLE DELTA WING DUE TO UNSTEADY VORTEX FLOWS
AIAA-2001-1329 Post-Buckling of Single and Multi-Bay Panels Using Strut, Strip and FE Methods