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