Paper
24 August 2009 Numerical and experimental investigation of an angle-ply laminate with a centre hole under tension load
J. T. Ruan, G. H. Zhao, J. W. Tong, M. Shen, S. B. Wang, P. Priolo, F. Aymerich
Author Affiliations +
Proceedings Volume 7375, ICEM 2008: International Conference on Experimental Mechanics 2008; 73750A (2009) https://doi.org/10.1117/12.839013
Event: International Conference on Experimental Mechanics 2008 and Seventh Asian Conference on Experimental Mechanics, 2008, Nanjing, China
Abstract
The stress-strain fields for composite laminate [±25]S4 containing a circular hole under uniform axial extension are investigated using numerical and experimental methods in this paper. The distributions of normal strain along the length direction around the hole on the specimen surface are measured using digital speckle correlation method (DSCM). Meanwhile, only the middle part of the laminate is taken into account to perform finite element (FE) analysis. For the side face of specimen, a tiny area (1.8mm x 2.4mm) over the hole is chosen to measure the normal strain and shear strain. The experimental results are in a good agreement with FE simulation. Additionally, the interlaminar stress analysis on the hole edge has been performed by FE method.
© (2009) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
J. T. Ruan, G. H. Zhao, J. W. Tong, M. Shen, S. B. Wang, P. Priolo, and F. Aymerich "Numerical and experimental investigation of an angle-ply laminate with a centre hole under tension load", Proc. SPIE 7375, ICEM 2008: International Conference on Experimental Mechanics 2008, 73750A (24 August 2009); https://doi.org/10.1117/12.839013
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KEYWORDS
Composites

Finite element methods

Interfaces

Speckle

3D modeling

Speckle pattern

Stress analysis

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