Optimal design of composite lattice shell structures for aerospace applications
Optimal design of composite lattice shell structures for aerospace applications
Optimal design of composite lattice shell structures for aerospace applications
In-Plane Response of Laminates with Spatially Varying Fiber Orientations: Variable Stiffness Concept
Retrieving Variable Stiffness Laminates from Lamination Parameters Distribution
Buckling Analysis of Geodesically Stiffened Composite Panels with Discrete Stiffeners
Virtual Testing of Glare Coupons Using Progressive Failure Analysis
Virtual Testing of Glare Coupons Using Progressive Failure Analysis
A Genetic Algorithm Based Blending Scheme for Design of Multiple Composite Laminates
Maximising Buckling Loads of Variable Stiffness Shells Using Lamination Parameters
Isogeometric Sizing and Shape Optimization of Beam Structures
Formulation of Composite Laminate Robustness Constraint in Lamination Parameters Space
Analysis of tow placed, parallel fiber, variable stiffness laminates
Analysis of Tow Placed, Parallel Fiber, Variable Stiffness Laminates
On the Effect of Geometric Nonlinearities on Static Load Alleviation
Simulation of Low-Velocity Impact Damage on Composite Laminates
Modal Testing of a Composite Cylinder with Circumferentially Varying Stiffness
Domain Decomposition and Interlaminar Stress Recovery of Multilayer Composite Structures
A New Scheme for the Optimum Design of Stiffened Composite Panels with Geometric Imperfections
A New Koiter Asymptotic Analysis for Buckling-Sensitive Structures
Stiffness Optimization of Composite Wings with Aeroelastic Constraints
Stiffness Optimization of Composite Wings with Aeroelastic Constraints
AIAA-2004-1720 Topology Design of Active Trusses with Energy Constraint
Design of Anisotropic Composite Shells Using an Isogeometric Approach
Maximum Buckling Load Design of General Cross-Section Cylinders Using Lamination Parameters
Tailoring for Strength of Steered-Fiber Composite Panels with Cutouts