Pages that link to "Item:Q1291469"

The following pages link to Parametrization in laminate design for optimal compliance (Q1291469):

Displaying 21 items.

• Global laminate optimization on geometrically partitioned shell structures (Q381570) (← links)
• Maximum stiffness and minimum weight optimization of laminated composite beams using continuous fiber angles (Q381589) (← links)
• A material optimization model to approximate energy bounds for cellular materials under multiload conditions (Q438445) (← links)
• Optimization of the reinforcement of a 3{D} medium with thin composite plates (Q438481) (← links)
• Designing the elastic properties of laminates as an optimisation problem: a unified approach based on polar tensor invariants (Q445464) (← links)
• On simultaneous shape and orientational design for eigenfrequency optimization (Q445510) (← links)
• Optimal orthotropy for minimum elastic energy by the polar method (Q644708) (← links)
• Failure optimization of geometrically linear/nonlinear laminated composite structures using a two-step hierarchical model adaptivity (Q658262) (← links)
• A note on design of fiber-nets for maximum stiffness (Q702333) (← links)
• On design of fiber-nets and orientation for eigenfrequency optimization of plates (Q835447) (← links)
• Stiffness and strength optimization of the anisotropy distribution for laminated structures (Q887100) (← links)
• Extremal overall elastic response of polycrystalline materials (Q1589290) (← links)
• Influence of invariant material parameters on the flexural optimal design of thin anisotropic laminates (Q1953284) (← links)
• Convex or non-convex? On the nature of the feasible domain of laminates (Q2224653) (← links)
• A note on the elastic and geometric bounds for composite laminates (Q2377184) (← links)
• Optimization of combining fiber orientation and topology for constant-stiffness composite laminated plates (Q2420805) (← links)
• Isogeometric design of anisotropic shells: optimal form and material distribution (Q2450009) (← links)
• A bi-value coding parameterization scheme for the discrete optimal orientation design of the composite laminate (Q2911857) (← links)
• On feasible regions of lamination parameters for lay-up optimization of laminated composites (Q3561890) (← links)
• A two-level procedure for the global optimum design of composite modular structures -- application to the design of an aircraft wing (Q5970621) (← links)
• Proper generalized decomposition solutions for composite laminates parametrized with fibre orientations (Q6042213) (← links)