A two-level procedure for the global optimum design of composite modular structures -- application to the design of an aircraft wing

DOI10.1007/s10957-012-0067-9zbMath1255.90099OpenAlexW3163492950MaRDI QIDQ5970621

Paolo Vannucci, Angela Vincenti, Marco Montemurro

Publication date: 29 January 2013

Published in: Journal of Optimization Theory and Applications (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10957-012-0067-9

zbMATH Keywords

genetic algorithmscomposite materialslaminatespolar method

Mathematics Subject Classification ID

Applications of mathematical programming (90C90) Nonconvex programming, global optimization (90C26) Approximation methods and heuristics in mathematical programming (90C59)

Related Items (9)

The Polar-Isogeometric Method for the Simultaneous Optimization of Shape and Material Properties of Anisotropic Shell Structures ⋮ A note on the elastic and geometric bounds for composite laminates ⋮ The design of laminates as a global optimization problem ⋮ Stiffness and strength optimization of the anisotropy distribution for laminated structures ⋮ A general hybrid optimization strategy for curve fitting in the non-uniform rational basis spline framework ⋮ Stacking sequence and shape optimization of laminated composite plates via a level-set method ⋮ Multi-scale least-weight design of a wing-box through a global/local modelling approach ⋮ Anisotropy and shape optimal design of shells by the polar-isogeometric approach ⋮ An alternative to the Kelvin decomposition for plane anisotropic elasticity

Uses Software

• BIANCA
• VICONOPT

Cites Work

• Unnamed Item
• Designing the elastic properties of laminates as an optimisation problem: a unified approach based on polar tensor invariants
• BIANCA: a genetic algorithm to solve hard combinatorial optimisation problems in engineering
• Plane anisotropy by the polar method
• Parametrization in laminate design for optimal compliance
• A two-level procedure for the global optimum design of composite modular structures -- application to the design of an aircraft wing
• Influence of invariant material parameters on the flexural optimal design of thin anisotropic laminates
• On higher-order differentiation in nonlinear mechanics
• Improved genetic algorithm for the design of stiffened composite panels
• Stiffness design of laminates using the polar method

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