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

DOI10.1007/s10957-012-0070-1zbMath1255.90098OpenAlexW1577058749MaRDI QIDQ1934621

Marco Montemurro, Angela Vincenti, Paolo Vannucci

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/s10957-012-0070-1

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 (11)

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 ⋮ Harmonic factorization and reconstruction of the elasticity tensor ⋮ 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 ⋮ A two-level procedure for the global optimum design of composite modular structures -- application to the design of an aircraft wing ⋮ An alternative to the Kelvin decomposition for plane anisotropic elasticity

Uses Software

• BIANCA

Cites Work

• 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
• Theoretical and numerical constraint-handling techniques used with evolutionary algorithms: A survey of the state-of-the-art
• Improved genetic algorithm for the design of stiffened composite panels
• Stiffness design of laminates using the polar method
• Unnamed Item

This page was built for publication: A two-level procedure for the global optimum design of composite modular structures -- application to the design of an aircraft wing