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Mesh Convergence Requirements for Composite Damage ModelsThe ability of the finite element method to accurately represent the response of objects with intricate geometry and loading renders the finite element method as an extremely versatile analysis technique for structural analysis. Finite element analysis is routinely used in industry to calculate deflections, stress concentrations, natural frequencies, buckling loads, and much more. The method works by discretizing complex problems into smaller, simpler approximations that are valid over small uniform domains. For common analyses, the maximum size of the elements that can be used is often be determined by experience. However, to verify the quality of a solution, analyses with several levels of mesh refinement should be performed to ensure that the solution has converged. In recent years, the finite element method has been used to calculate the resistance of structures, and in particular that of composite structures. A number of techniques such as cohesive zone modeling, the virtual crack closure technique, and continuum damage modeling have emerged that can be used to predict cracking, delaminations, fiber failure, and other composite damage modes that lead to structural collapse. However, damage models present mesh refinement requirements that are not well understood. In this presentation, we examine different mesh refinement issues related to the representation of damage in composite materials. Damage process zone sizes and their corresponding mesh requirements will be discussed. The difficulties of modeling discontinuities and the associated need for regularization techniques will be illustrated, and some unexpected element size constraints will be presented. Finally, some of the difficulties in constructing models of composite structures capable of predicting transverse matrix cracking will be discussed. It will be shown that to predict the initiation and propagation of transverse matrix cracks, their density, and their saturation may require models that are significantly more refined than those that have been contemplated in the past.
Document ID
20160007808
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Davila, Carlos G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
June 22, 2016
Publication Date
March 17, 2016
Subject Category
Composite Materials
Report/Patent Number
NF1676L-23575
Report Number: NF1676L-23575
Meeting Information
Meeting: Mechanical Engineering Seminar at Eindhoven University of Technology
Location: Eindhoven
Country: Netherlands
Start Date: March 17, 2016
Sponsors: Eindhoven Univ. of Technology
Funding Number(s)
WBS: WBS 544163.04.01.07.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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