Experiences with Minimum Weight Design of Structures Using Optimality Criteria Methods
High Altitude Long Endurance Aircraft Design Studies
A Study of the Space Station `Freedom' Response to the Disturbance Environment (AAS 93-643)
Vulnerability Analysis of Aircraft Fuselage Subjected to Internal Detonations
Analytical Simulation of Internal Explosions in Commercial Aircraft
Ply Orientation as a Variable in Aeroelastic Optimization
Flutter Instability Tracking for Aeroelastic Design Optimization Studies