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Werkstoff
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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
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