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2003-01-0576 A Study on the Bending Springback of Aluminum Alloy 5754
A Comprehensive Nonlinear Model for Sandwich-Shells with Anisotropic Faces and Compressible Core
Active Aeroelastic Control of 2-D Wing-Flap Systems in an Incompressible Flowfield
Aeroelastic Characteristic of an Airfoil Containing Laminated Composite Plate (AIAA 2014-1196)
AIAA-2001-1182 Progressive Failure Studies of Composite Panels With and Without Cutouts
AIAA-2001-1188 Post-Buckling Analysis of Debonded Sandwich Beams
AIAA-2001-1459 Volterra Series Approach for Nonlinear Aeroelastic Response of 2-D Lifting Surfaces
AIAA-2001-1490 Optimum Design for Double-Lap Bolted Composite Joints Using a Genetic Algorithm
AIAA-2004-1559 Global-Local Finite Element Analysis of Bonded Single-Lap Joints
AIAA-2004-1560 Nonlinear Analysis of Bonded Composite Single-Lap Joints
AIAA-2004-1595 Progressive Failure of Composite Laminates Using LaRC02 Criteria
AIAA-2004-1673 Aeroelastic Response of Flapped Wing Systems Using Robust Estimation Methodology
AIAA-2004-1926 Impact Response of Sandwich Beams with Functionally Graded Core
AIAA-2004-2046 Aeroelastic Response of Composite Aircraft Swept Wings Impacted by a Laser Beam
AIAA-2004-2049 Thin-Walled Rotating Composite Blades Featuring Extension-Twist Elastic Coupling
AIAA-2006-1641 Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVs
AIAA-2006-1701 Static, Buckling and Dynamic Behavior of Inflatable Beams
AIAA-2006-1731 Aerothermoelastic Stability of Composite Aircraft Wings Subjected to Heat Inputs
AIAA-2006-1739 Dynamics of Thin-Walled Composite Aircraft Wings Carrying External Stores
AIAA-2006-1823 Design and Shape Optimization of Inflatable Wings
AIAA-2006-1835 Time-Delayed Feedback Control of a 2-D Supersonic Flapped Wings
AIAA-2006-1836 Robust Aeroelastic Control of 2-D Supersonic Flapped Lifting Surfaces
AIAA-2006-1872 Modeling, Vibration and Instability of an Advanced Tiltrotor-Wing System
AIAA-2006-1963 Thermo-Mechanical Analysis of Bonded Cylindrically Curved Composite Shell Structures
AIAA-2006-2107 Free Vibration of Doubly-Curved Sandwich Panels with Laminated Face Sheets
AIAA-2006-2110 Localized Magnetoelastic Bending Vibration of an Electroconductive Elastic Plate
AIAA-2006-2161 Aeroelastic Behavior of a Non-Rigidizable Inflatable UAV Wing
AIAA-2006-2186 Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings
AIAA-2006-2267 Analysis of Brazed Single-Lap Joints by Peridynamics Theory
AIAA-2006-2270 Validated Analysis Method for Bolted Composite Lap Joints
Analysis of a 2-D Supersonic Lifting Surface with Time Delayed Feedback Control
Analysis of Bolted-Bonded Composite Lap Joints AIAA Paper 2007-2187 CD-ROM Number 7