Stiffness and strength optimization of the anisotropy distribution for laminated structures

DOI10.1007/s10957-014-0693-5zbMath1327.74046OpenAlexW2071757721MaRDI QIDQ887100

Boris Desmorat, Paolo Vannucci, Anita Catapano

Publication date: 28 October 2015

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

Full work available at URL: https://doi.org/10.1007/s10957-014-0693-5

zbMATH Keywords

anisotropypolar methodstiffness and strength optimization

Mathematics Subject Classification ID

Classical linear elasticity (74B05) Anisotropy in solid mechanics (74E10) Optimization of other properties in solid mechanics (74P10) Compliance or weight optimization in solid mechanics (74P05)

Related Items (4)

The Polar-Isogeometric Method for the Simultaneous Optimization of Shape and Material Properties of Anisotropic Shell Structures ⋮ Static analysis of anisotropic doubly-curved shells with arbitrary geometry and variable thickness resting on a Winkler-Pasternak support and subjected to general loads ⋮ Strength optimisation of variable angle-tow composites through a laminate-level failure criterion ⋮ Anisotropy and shape optimal design of shells by the polar-isogeometric approach

Uses Software

• BIANCA
• ZAERO

Cites Work

• Unnamed Item
• Aeroelastic tailoring using fiber orientation and topology optimization
• 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
• Existence and uniqueness of solutions of (\(k+2\))-point nonlocal boundary value problems for ordinary differential equations
• Optimal orthotropy for minimum elastic energy by the polar method
• The polar analysis of a third-order piezoelectricity-like plane tensor
• Plane anisotropy by the polar method
• Problems and methods of optimal structural design. Transl. from the Russian by Vadim Komkov, ed. by Edward J. Haug
• A two-level procedure for the global optimum design of composite modular structures -- application to the design of an aircraft wing
• A note on the elastic and geometric bounds for composite laminates
• Mathematical Models for Elastic Structures
• Invariant formulation of phenomenological failure criteria for orthotropic sheets and optimisation of their strength
• A theory of the yielding and plastic flow of anisotropic metals
• A two-level procedure for the global optimum design of composite modular structures -- application to the design of an aircraft wing

This page was built for publication: Stiffness and strength optimization of the anisotropy distribution for laminated structures