Published February 5, 2026 | Version 0.8.5
Software Open

Methods for analysis and design of composites

Authors/Creators

  • 1. Delft University of Technology

Description

High-performance module to calculate properties of laminated composite materials. Usually, this module is used to calculate: * A, B, D, E, F, H plane-stress stiffness matrices - A, B, D, for classical plate theory (CLT, or CLPT) - A44, A45, A55 for first-order shear deformation theory (FSDT) - E, F, H for third-order shear deformation theory (TSDT) * Material invariants, trace-normalized or not * Lamination parameters based on material invariants * Stiffness matrices (ABD) based on lamination parameters

Notes

Please, cite this software using: Saullo G. P. Castro (2026). Methods for analysis and design of composites (Version 0.8.5). Zenodo. DOI: https://doi.org/10.5281/zenodo.2871782

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saullocastro/composites-0.8.5.zip

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