Compressive Strength Following Delamination Induced Interaction of Panel and Sublaminate Buckling
Conceptual design optimization of composite wings with aeroelastic and strength constraints
Conceptual Design Optimization of Composite Wings with Aeroelastic and Strength Constraints
Damage Resistance and Damage Tolerance of Hybrid Carbon-Glass Laminates
Damage Tolerance of Buckling Optimized Variable Angle Tow Panels
Evaluation of a General Aviation Flight Data Recorder AIAA Paper
FAA's Wide Area Augmentation System (WAAS) System Summary of Cross-Country Flight Test
Fatigue of Metal-Composite Joints with Penetrative Reinforcement
Free vibration and flutter sensitivity analyses of a large transport aircraft
Free Vibration and Flutter Sensitivity Analyses of a Large Transport Aircraft
Gust Alleviation and Flutter Suppression of an Optimized Composite Wing with Active Control
Maximizing Compression after Impact Strength of Uncoupled Symmetric and Non-Symmetric Laminates
Methodologies and Tools to Support the Architecting of Complex Helicopter Avionics Systems