Stiffness design of laminates using the polar method
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Publication:5956755
DOI10.1016/S0020-7683(01)00177-9zbMath1016.74019MaRDI QIDQ5956755
Publication date: 20 August 2003
Published in: International Journal of Solids and Structures (Search for Journal in Brave)
inverse problemselastic anisotropic laminasparticular solutionspolar representation methodquasi-homogeneitythermo-mechanical properties
Related Items (16)
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 ⋮ Strange Laminates ⋮ Harmonic factorization and reconstruction of the elasticity tensor ⋮ Plane anisotropy by the polar method ⋮ The design of laminates as a global optimization problem ⋮ General theory of coupled thermally stable anisotropic laminates ⋮ A two-level procedure for the global optimum design of composite modular structures -- application to the design of an aircraft wing ⋮ Computation of minimal covariants bases for 2D coupled constitutive laws ⋮ Invariant measures of the lack of symmetry with respect to the symmetry groups of 2D elasticity tensors ⋮ Designing the elastic properties of laminates as an optimisation problem: a unified approach based on polar tensor invariants ⋮ A unified approach to invariants of plane elasticity tensors ⋮ Continuous anisotropic damage as a twin modelling of discrete bi-dimensional fracture ⋮ Anisotropy and shape optimal design of shells by the polar-isogeometric approach ⋮ Minimal functional bases for elasticity tensor symmetry classes ⋮ A two-level procedure for the global optimum design of composite modular structures -- application to the design of an aircraft wing
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