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CPA: Composite Property Analysis

Simulations Index (at Interactive Learning Tools subsite)

This program uses micro-mechanical models to predict the anisotropic thermoelastic properties for a variety of composite materials. Properties predicted include Young's moduli (E11, E22, and E33), shear moduli (G12, G13, and G23), Poisson's ratios (n12, n13, and n23), and coefficients of thermal expansion.
This work was conducted in a joint effort between the University of Delaware and Michigan State University under the aegis of the National Science Foundation project "Manufacturing Education and Training Program in Composite Materials for the DoD and Durable Goods Industries" as part of the DARPA Supplementary Education Awards.

Background

Various types of composites can be distinguished by the shape (or aspect ratio) and state of orientation of the reinforcing fibers induced by processing conditions. The types of composites treated include
  • Continuous-fiber lamina
  • Chopped-fiber sheet molding materials
  • Extrusions
  • Short-fiber bulk molding materials
  • Platelet-reinforced materials
Predicted properties can be displayed in tabular or graphical form.

Features

The introductory page describes the program and presents the user with three options: Tutorial (which provides an explanation of the various aspects of composite materials), Theoretical Basis (which describes the theoretical basis and provides references), and Computation. Selection of the Computation option leads to the input page shown below.

complex-shape LIMS output

The user may select the units to be used, choose between a two-component resin/fiber or three-component resin/fiber/filler compound, and elect to use volume fraction or weight fraction concentration variables. A variety of common resins, fibers, and fillers can be selected from the pulldown menus. The appropriate data for these materials is stored in the program database.

The user may also enter properties for materials not included in the database. A variety of microstructures associated with various types of composites are accessed through the pulldown window for select microstructures. The user enters a value for the aspect ratio and the orientation parameters. Selection of certain microstructures fixes some of the orientation parameters. The user may select from various output modes. If the plot options are selected, the user may choose which of the thermoelastic properties to view.

Help buttons are associated with key data. Selection of the associated help button will display that portion of the tutorial related to the selection.

Applications

complex-shape LIMS output
The program yields predictions for the complete set of thermoelastic properties. This capability is particularly useful, since full experimental characterization is not always feasible. The most important application is sensitivity studies investigating the influence of constituent properties-composition, aspect ratio, and process-induced fiber orientation-on the thermoelastic properties.

This feature enables the user to select, design, or investigate the feasibility of using composite materials to meet stiffness-dominated design constraints. An interesting feature is the ability to display the directional dependence of the properties for off-axis loading. The polar plot displayed here shows the shear modulus, G12, at various off-axis loading angles for a sheet molding material with partial fiber alignment.

Prof. John W. Gillespie Jr.

phone: 302-831-8702
fax: 302-831-8525
e-mail: gillespie@ccm.udel.edu


Center for Composite Materials
201 Composites Mfg. Science Lab
University of Delaware
Newark, DE 19716-3144

phone: 302-831-8149
fax: 302-831-8525
e-mail: info@ccm.udel.edu

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