Abstract

This paper studies the influence of displacement rate on mode II delamination of unidirectional carbon/epoxy composites. End-notched flexure test is performed at displacement rates of 1, 10, 100 and 500 mm/min. Experimental results reveal that the mode II fracture toughness GIIC increases with the displacement, with a maximum increment of 45% at 100 mm/min. In addition, scanning electron micrographs depict that fiber/matrix interface debonding is the major damage mechanism at 1 mm/min. At higher speeds, significant matrix-dominated shear cusps are observed contributing to higher GIIC. Besides, it is demonstrated that the proposed rate-dependent model is able to fit the experimental data from the current study and the open literature generally well. The mode II fracture toughness measured from the experiment or deduced from the proposed model can be used in the cohesive element model to predict failure. Good agreement is found between the experimental and numerical results, with a maximum difference of 10%. The numerical analyses indicate crack jump occurs suddenly after the peak load is attained, which leads to the unstable crack propagation seen in the experiment.

Highlights

  • Delamination is one of the major failure mechanisms in composite laminates due to their low interlaminar strength [1,2,3,4]

  • For composite materials used in aeronautical applications, barely visible impact damage (BVID) could be generated under low energy impact loading [5]

  • BVID could happen at lamina level as well [6]

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Summary

Introduction

Delamination is one of the major failure mechanisms in composite laminates due to their low interlaminar strength [1,2,3,4]. For composite materials used in aeronautical applications, barely visible impact damage (BVID) could be generated under low energy impact loading [5]. BVID could happen at lamina level as well [6]. The mode II shearing mode is important as large through-thickness shear stresses are induced due to bending of the composite structures [1]. The material response and properties of polymeric materials are commonly known to be rate-dependent [7,8]. It is essential to understand the influence of loading speed on mode II interlaminar fracture toughness

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