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Werkstoff
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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
Low-Speed Impact Response Characteristics of Composite Sandwich Panels
AIAA-2001-1188 Post-Buckling Analysis of Debonded Sandwich Beams
Development of a Pressure Box to Evaluate Reusable-Launch-Vehicle Cryogenic-Tank Panels
Implications of External Stores on Static and Dynamic Aeroelasticity of Advanced Aircraft Wings
Effect of Curvature on the Impact Damage Characteristics and Residual Strength of Composite Plates
Optimal Design of Grid-Stiffened Composite Panels Using Global and Local Buckling Analyses
Effect of Elastic Couplings on Dynamics and Instability of Anisotropic Spinning Thin-Walled Beams
Buckling Analysis of General Triangular Anisotropic Plates Using Polynomials
Active Aeroelastic Control of 2-D Wing-Flap Systems in an Incompressible Flowfield
Nonlinear Analysis of a Bonded Patch Repair of a Skin with a Cutout
Circular Cylindrical Shells Immersed in a Magnetic Field: Modeling and Dynamic Behavior
Core and Face Sheet Anisotropy in Deformation and Buckling of Sandwich Panels