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Journal ArticleDOI

The Influence of Stacking Sequence on Laminate Strength

N. J. Pagano, +1 more
- 01 Jan 1971 - 
- Vol. 5, Iss: 1, pp 50-57
TLDR
In this article, an approach is presented to predict the detailed stacking sequence of specific layer orientations which leads to optimum protection against delamination under uniaxial static and fatigue loadings.
Abstract
Based upon considerations relating to the nature of the interlaminar stresses in composite laminates, an approach is presented to predict the detailed stacking sequence of specific layer orientations which leads to optimum protection against delamination under uniaxial static and fatigue loadings. In particular, it is argued that the interlaminar normal stress as well as the interlaminar shear stress, is instrumental in precipitating delamination and subsequent strength degradation. Correlation with existing experimental evidence of the stacking sequence phenomenon is presented.

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Citations
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Journal ArticleDOI

On the Analysis and Design of the End Notched Flexure (ENF) Specimen for Mode II Testing

TL;DR: In this article, an end notched flexure (ENF) specimen is examined as a candidate for measuring interlaminar fracture toughness in skew symmetric loading and a simple design study for sizing the ENF specimen to minimize geometric nonlinear response and to avoid nonlinear material behavior or flexural failure is presented.
Journal ArticleDOI

Damage Tolerance of Laminated Composites Containing an Open Hole and Subjected to Compressive Loadings: Part I—Analysis

TL;DR: In this paper, an analytical investigation was performed to study the damage in laminated composites containing an open hole and subjected to compressive loading, and a progressive damage model was developed during t...
Journal ArticleDOI

Stress fields in composite laminates

TL;DR: In this article, a new theory is proposed to define the complete stress field within an arbitrary composite laminate, based upon an extension of Reissner's variational principle to laminated bodies.
Journal ArticleDOI

Experimental studies of thin-ply laminated composites

TL;DR: In this paper, a new processing method was developed for spreading fiber tows to make thin-ply laminated composites, which is robust and easy compared with other available thinply methods.
BookDOI

Mechanical testing of advanced fibre composites

TL;DR: In this paper, the authors present a method for testing organic matrix composites using tension compression shear, flexure through-thickness testing, fracture toughness, impact and damage tolerance.
References
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Journal ArticleDOI

Interlaminar Stresses in Composite Laminates Under Uniform Axial Extension

TL;DR: In this article, the response of a finite-width composite laminate under uniform axial strain is treated through the application of classical elasticity theory, and finite-difference solution techniques are employed to obtain solutions for stresses and displacements throughout the region.
Journal ArticleDOI

Interlaminar Shear in Laminated Composites Under Generalized Plane Stress

TL;DR: In this article, an analysis of interlaminar shear stresses is performed for a laminate under generalized plane stresses, where the laminate is modeled as a set of anisotropic layers separated by isotropic adhesive layers.
Journal ArticleDOI

Geometric Design of Composite Cylindrical Characterization Specimens

TL;DR: In this paper, a procedure is outlined to determine the proper geometry of anisotropic and laminated cylinders such that elastic stress gradients can be reduced to a predetermined limit, which consists of combining a modified plane strain elasticity solu tion with shell theory.
Journal ArticleDOI

Bending and Stretching of Laminated Aeolotropic Plates

TL;DR: In this article, a linear theory is established for general multilayer aeolotropic plate subject to in-plane forces and transverse loading, and it is shown that coupling phenomenon occurs, between in plane forces and cross-verse bending, in differential equations as well as in boundary conditions.
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