journal article·2013-02

Size effects on the tensile and compressive failure of notched composite laminates

G.H. Erçin, P.P. Camanho, J. Xavier, G. Catalanotti, S. Mahdi, P. Linde

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Abstract

An experimental and analytical investigation of the effect of size on the strength of composite laminates with central holes loaded in tension and compression is presented. Specimens with different hole sizes and with constant width-to-diameter ratios were tested in tension and compression under quasi-static loading and the strength reduction for increasing sizes was quantified for two lay-ups and for the two loading conditions. The first-ply failure load of the outer ply was identified using a new method that post-processes the displacement field obtained using the digital image correlation technique. The accuracy of the available strength prediction methods (point and average stress methods, inherent flaw model, semi-analytical cohesive zone model and finite fracture mechanics) to simulate the effect of size on the strength of notched composites is discussed. It is shown that the finite fracture mechanics model is the most accurate method.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Mechanical Behavior of Composites · Composite Structure Analysis and Optimization · Textile materials and evaluations

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (18)

Show source-provided references
1. Stress fracture criteria for laminated composites containing stress concentrations10.1177/002199837400800303 ↗
2. An experimental investigation into the tensile strength scaling of notched composites10.1016/j.compositesa.2006.07.008 ↗
3. Damage progression by the element-failure method (EFM) and strain invariant failure theory (SIFT)10.1016/j.compscitech.2004.10.022 ↗
4. Prediction of size effects in notched laminates using continuum damage mechanics10.1016/j.compscitech.2007.02.005 ↗
5. Macroscopic fracture mechanics of advanced composite materials10.1177/002199837100500402 ↗
6. Failure prediction technique for compression loaded carbon fibre-epoxy laminate with open holes10.1177/002199839102501106 ↗
7. A finite fracture mechanics model for the prediction of the open-hole strength of composite laminates10.1016/j.compositesa.2012.03.004 ↗
8. Bistable composite laminates: Effects of laminate composition on cured shape and response to thermal load10.1016/j.compstruct.2009.08.043 ↗
9. ARAMIS Commercial Software v6.1, GOM mbH. August 7, 2009.
10. Measuring displacement fields by cross-correlation and a differential technique: experimental validation10.1117/1.OE.51.4.043602 ↗
11. Standard test method for tensile properties of polymer matrix composite materials, ASTM D 3039/D 3039M-00. West Conshohocken (PA, USA): American Society for Testing and Materials (ASTM); July 2000.
12. Static compression failure of carbon fibre T800/924C composite plate with a single hole10.1177/002199839002400505 ↗
13. Open hole tensile strength of polymer composite laminates, ASTM D 5766/D 5766M-02a. West Conshohocken (PA, USA): American Society for Testing and Materials (ASTM); February 2003.
14. MATLAB 7.12.0 (R2011a) Software, MatWorks Inc., March 18, 2011.
15. Prediction of in situ strengths and matrix cracking in composites under transverse tension and in-plane shear10.1016/j.compositesa.2005.04.023 ↗
16. Standard test method for open-hole compressive strength of polymer matrix composite laminates, ASTM D 6484/D 6484M-09. West Conshohocken (PA, USA): American Society for Testing and Materials (ASTM); March 2004.
17. Compressive behaviour of composites – Report 94
18. Sutcliffe MPF, Xin XJ, Fleck NA, Curtis PT. Composite compressive strength modeller. Engineering Department, Cambridge University, Cambridge, CB2 1PZ, UK. DERA Farnborough, GU14 0LW, UK: Structural Materials Centre; 1999.