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Journal ArticleDOI

Stress and failure analysis of mechanically fastened joints in composite laminates

Marie-Laure Dano, +2 more
- 01 Nov 2000 - 
- Vol. 50, Iss: 3, pp 287-296
TLDR
In this article, a finite-element model is developed to predict the response of pin-loaded composite plates, taking into account contact at the pinhole interface, progressive damage, large deformation theory, and a non-linear shear stress-strain relationship.
About
This article is published in Composite Structures.The article was published on 2000-11-01. It has received 166 citations till now. The article focuses on the topics: Composite laminates & Stress–strain curve.

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Citations
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Journal ArticleDOI

A review: Fibre metal laminates, background, bonding types and applied test methods

TL;DR: In this article, the most commercially available fiber metal laminates (FMLs) are ARALL (Aramid Reinforced Aluminium Laminate), based on aramid fibres, GLARE (Glass Reinforced Aluminum Laminate) based on high strength glass fibres and CARALL (Carbon Reinforced Alloy Laminate, based on carbon fibres).
Journal ArticleDOI

Advances in strength theories for materials under complex stress state in the 20th Century

TL;DR: A survey of the advances in strength theory (yield criteria, failure criterion, etc) of materials (including matellic materials, rock, soil, concrete, ice, iron, polymers, energetic material etc) under complex stress was presented in this paper.
Journal ArticleDOI

Strength prediction of bolted joints in graphite/epoxy composite laminates

TL;DR: In this article, a parametric finite element analysis was conducted to investigate the effect of failure criteria and material property degradation rules on the tensile behaviour and strength of bolted joints in graphite/epoxy composite laminates.
Journal ArticleDOI

Experimental investigation of a novel hybrid metal–composite joining technology

TL;DR: In this paper, an integrative joining technology between steel and carbon fiber reinforced plastics (CFRP) is presented for lightweight design applications in aviation industries, where small spikes are welded onto metal surfaces via "cold-metal transfer" which then build up a fibre-friendly fixation through form-closure with co-cured composites.
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CFRP/titanium hybrid material for improving composite bolted joints

TL;DR: In this paper, the authors demonstrate the influence of titanium hybridization on specific characteristics of CFRP-materials, thus proving the mechanical potential of composite composite joints when used as an advanced reinforcement technique for highly loaded composite joints.
References
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Journal ArticleDOI

A Progressive Damage Model for Laminated Composites Containing Stress Concentrations

TL;DR: In this article, a progressive damage model for notched laminated composites subjected to tensile loading is presented, which is capable of assessing damage in laminates with arbitrary ply-orientations and of predicting the ultimate tensile strength of the notched Laminates.
Journal ArticleDOI

Nonlinear Elastic Behavior of Unidirectional Composite Laminae

TL;DR: In this paper, complementary elastic energy density is used to derive a stress-strain relation, which is linear in uniaxial loadings in the longitudinal and trans verse directions, but nonlinear in shear.
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Stress analysis and strength prediction of mechanically fastened joints in FRP: A review

TL;DR: A review of the investigations that have been made on the stress and strength analysis of mechanically fastened joints in fiber-reinforced plastics (FRP) is presented in this article, where the experimental observations of the effects of joint geometry, ply-orientation, lay-up and through-thickness pressure on the joint behaviour are described briefly for both single and multi-fastener joints.
Journal ArticleDOI

Analysis of Laminate Strength and Its Distribution

TL;DR: In this article, a failure criterion for a laminated composite is presented and a salient nature of this criterion is the use of "in situ shear strength" measured in the form of cross-ply laminate.
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