Recovery of Interlaminar Tensile Stresses in Curved Laminates Subject to Biaxial Flexure: The Case of an Elastically Induced Curvature Purposely Misaligned with the Principal Directions of Initial Curvature-Reference-Cited by-同舟云学术

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Recovery of Interlaminar Tensile Stresses in Curved Laminates Subject to Biaxial Flexure: The Case of an Elastically Induced Curvature Purposely Misaligned with the Principal Directions of Initial Curvature

Published:2024 Issue: Volume:52 Page:543-550
ISSN:2452-3216
Container-title:Procedia Structural Integrity
language:en
Short-container-title:Procedia Structural Integrity

Author:

Marchignoli Lorenzo,Bertocchi Enrico,Giacopini Matteo,Mangeruga Valerio

Publisher

Elsevier BV

Reference13 articles.

1. Complete transverse stress recovery model for linear shell elements in arbitrarily curved laminates;Daniel;Composite Structures,2020

2. Dassault System, 2006. Abaqus 6.6 Analysis Users's Manual. Abaqus Theory Manual

3. Thermal stresses in doubly-curved cross-ply laminates;Huang;International Journal of Solids and Structures,1992

4. Irons, B. M. R., 1976. ‘The semi-loof shell elements’ in Finite Element for Thin Shells and Curved Membranes. Eds. D. G. Ashwell and R. H. Gallagher

5. Model for interlaminar normal stress in singly curved laminates;Kress;Composite Structures,2005

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