AIAA-2001-1459 Volterra Series Approach for Nonlinear Aeroelastic Response of 2-D Lifting Surfaces
AIAA-2001-1182 Progressive Failure Studies of Composite Panels With and Without Cutouts
AIAA-2001-1188 Post-Buckling Analysis of Debonded Sandwich Beams
AIAA-2001-1490 Optimum Design for Double-Lap Bolted Composite Joints Using a Genetic Algorithm
Core and Face Sheet Anisotropy in Deformation and Buckling of Sandwich Panels
Nonlinear Vibration of Finitely Electroconductive Plate-Strips in a Magnetic Field
Optimal Control of Pretwisted Shearable Smart Composite Rotor Blades
Nonlinear Time Delayed Feedback Control of Aeroelastic Systems: A Functional Approach
Modeling the Structural Response of Multifunctional Materials: The In-field Vibration of Thin Plates
Full-Field Structural Response of Composite Structures: Analysis and Experiment
Active Aeroelastic Control of 2-D Wing-Flap Systems in an Incompressible Flowfield
Analysis of Bolted Laminates of Varying Thickness and Lay-Up with Metallic Inserts
Functionally Graded Sandwich Core with Arbitrary Variation in Properties
Buckling of Long, Thin Inflatable Cylinders Loaded in Axial Compression
Analysis of a 2-D Supersonic Lifting Surface with Time Delayed Feedback Control