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title: 31st Structures, Structural Dynamics and Materials Conference
Dynamics and Aeroelastic Analysis of Missiles
AIAA-2006-2105 Geometrically-Exact, Intrinsic Theory for Dynamics of Moving Composite Plates
A Historical Perspective on Rotary Wing Dynamics and Aeroelasticity
AIAA-2004-1837 Structural Optimization of Composite Rotor Blades
Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance Aircraft
On Static Stability of Damaged Columns
Stability Analysis of Columns with Imperfection
Investigation of the Effect of Damage Shape and Beam Shape Using a Unified Framework
Modeling Beams with Various Boundary Conditions Using Fully Intrinsic Equations
Asymptotic Beam Theory for Planar Deformation of Initially Curved Isotropic Strips
Effect of Engine Placement on Aeroelastic Trim and Stability of Flying Wing Aircraft
Enhancement of Roll Maneuverability Using Post-Reversal Design. Part I: Nonlinear Analysis
Rigorous Joining of Advanced Reduced-Dimensional Beam Models to 2-D Finite Element Models
Parametric Study of Joined-Wing Aircraft Geometry
AIAA-2006-1656 Modeling of Ground Vibration Testing for Highly Flexible Aircraft
AIAA-2006-1822 Coupling Global and Local Aspects of Cross-Sectional Optimization for Rotor Blades
Aeroelastic Stability of Composite Rotor Blades in Hover