Biaxial test results for strength and deformation of a range of E-glass and carbon fibre reinforced composite laminates: failure exercise benchmark data

By P. Soden, M. Hinton, A. Kaddour. 2002

295 citations recorded by the source corpus.

Subfields: Mechanics of Materials, Polymers and Plastics

View Paper: https://www.semanticscholar.org/paper/030113597f36eb0d7cd9ab21fa0c92afa830739d

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Mechanics of Materials

1. Pedro P. Camanho
2. G. Catalanotti
3. A. Arteiro
4. S. Pinho
5. C. Dávila
6. A. Melro
7. P. Robinson
8. M. Vogler

In Polymers and Plastics

1. A. Melro
2. S. Pinho
3. A. Long
4. P. Robinson
5. L. Iannucci
6. C. Dávila
7. Pedro P. Camanho

Citations in the corpus

• Composite materials non-linear modelling for long fibre-reinforced laminates (2008, result): “For validation purposes, the results of several numerical analyses are contrasted with experimental results found in the literature and with the experimental benchmark data [29] provided in the context of the ‘‘world-wide failure exercise’’.”
• High strain rate characterisation of unidirectional carbon-epoxy IM7-8552 in transverse compression and in-plane shear using digital image correlation (2010, result): “The above assumption is further supported by the biaxial longitudinal and shear loading data provided by Soden et al. (2002), which indicates that the in-plane shear strength is not significantly influenced by the presence of longitudinal compressive stresses for high ratios of X/r11.”
• Physically-based failure models and criteria for laminated fibre-reinforced composites with emphasis on fibre kinking: Part I: Development (2006, background): “Experimental results from the World Wide Failure Exercise (WWFE) [1,4] indicate that the (admittedly scarce) data on fibre tensile failure under bior multi-axial stress states does not seem to invalidate the maximum stress criterion.”
• Failure Criteria for FRP Laminates (2005, background): “Failure envelopes and WWFE test data [2] for unidirectional composite E-Glass/LY556.”
• A micromechanical study of residual stress and its effect on transverse failure in polymer–matrix composites (2006, background): “Experiments on biaxial failure envelopes for unidirectional fibre composites have focused on the combined longitudinal and transverse loading conditions (see Soden et al., 2002 ).”
• Three-dimensional invariant-based failure criteria for fibre-reinforced composites (2015, background): “…37.5 MPa Soden et al. (2002) σt22 u 17.5 MPa Soden et al. (2002) σt12 u 50.9 MPa Soden et al. (2002) YC -130.3 MPa Soden et al. (2002) σc22 u -43.8 MPa Soden et al. (2002) σc12 u 81.1 MPa Soden et al. (2002) SL 66.5 MPa Soden et al. (2002) 32 Table 6: E-Glass/MY750/HY917/DY063 material properties.”
• Failure Models and Criteria for Frp Under In-Plane or Three-Dimensional Stress States Including Shear Non-Linearity (2013, unknown): “[60,86] Material E11 E22 G12 SL Y T Y C αo (GPa ) (GPa ) (GPa ) (MPa ) (MPa ) (MPa ) (◦ ) E-Glass/LY556 53.”