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Werkstoff
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Compression After Impact Modeling of Damage Tolerant Composite Laminates
Buckling and Propagation of a Delaminated Composite Beam in Bending
Compressive Strength Following Delamination Induced Interaction of Panel and Sublaminate Buckling
Damage Tolerance of Buckling Optimized Variable Angle Tow Panels
Buckling Optimization of Variable Angle Tow Panels Using Exact Strip Models
Damage Resistance and Damage Tolerance of Hybrid Carbon-Glass Laminates
Maximizing Compression after Impact Strength of Uncoupled Symmetric and Non-Symmetric Laminates
Bimodal Buckling of Optimised Truss-Lattice Shear Panels AIAA Paper 2007-2122 CD-ROM Number 7
AIAA-2006-1787 Post-Buckling of Stiffened Composite Structures with Delaminations
AIAA-2004-1568 Post-Buckling and Fatigue Limit of Artificially Delaminated Composites
AIAA-2001-1329 Post-Buckling of Single and Multi-Bay Panels Using Strut, Strip and FE Methods
Optimum Design and Validation of Flat Composite Beams Subject to Frequency Constraints
Optimum Design of High Aspect Ratio Wings Subject to Aeroelastic Constraints
Nonlinear Modelling of Delaminated Struts