Table of Content

Open Access iconOpen Access

ARTICLE

Prediction of Delamination Onset and Critical Force in Carbon/Epoxy Panels Impacted by Ice Spheres

Jennifer D. Rhymer1, Hyonny Kim1

Dept. of Structural Engineering, University of California San Diego, La Jolla, CA 92093 USA

Computers, Materials & Continua 2013, 35(2), 87-117. https://doi.org/10.3970/cmc.2013.035.087

Abstract

Polymer matrix composite structures are exposed to a variety of impact threats including hail ice. Internal delamination damage created by these impacts can exist in a form that is visually undetectable. This paper establishes an analysis methodology for predicting the onset of delamination damage in toughened carbon/epoxy composite laminates when impacted by high velocity ice spheres (hailstones). Experiments and analytical work focused on ice sphere impact onto composite panels have determined the failure threshold energy as a function of varying ice diameter and panel thickness, and have established the ability to predict the onset of delamination using cohesive elements in explicit dynamic finite element analysis. A critical force associated with damage onset was found to be independent of the ice diameter and thus can be expressed as a function of basic panel-describing parameters, namely bending rigidity and interlaminar fracture energy. Critical force can be used as a failure criterion in simpler models (e.g., shell elements) when predicting the onset of delamination by high speed spherical ice impact.

Keywords


Cite This Article

J. D. Rhymer and H. Kim, "Prediction of delamination onset and critical force in carbon/epoxy panels impacted by ice spheres," Computers, Materials & Continua, vol. 35, no.2, pp. 87–117, 2013. https://doi.org/10.3970/cmc.2013.035.087



cc This work is licensed under a Creative Commons Attribution 4.0 International License , which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
  • 1777

    View

  • 1606

    Download

  • 0

    Like

Share Link