Materials Algorithms Project Composites: Program Library

This library contains complete PROGRAMS for the modelling and analysis of properties and phenomena associated with composites, laminates and coatings.

Format of documentation within this library.

Programs Available

A

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B

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C

MAP_COMP_COAXCY

This program calculates the radial distribution of axial, radial and hoop stresses in a series of coaxial cylinders (the inner cylinder being solid), due to a temperature change from the initial (stress-free) state and/or an externally applied axial and/or radial stress.

Language: Executable file only.

MAP_COMP_COSTCY

This program calculates the through-thickness stress distribution resulting from progressive deposition of a coating onto a hollow, cylindrical substrate, for a specified deposition stress and subsequent temperature change.

Language: Executable file only.

MAP_COMP_COSTPL

This program calculates the through-thickness distribution of (in-plane) stresses resulting from progressive deposition of a coating onto a planar substrate for a specified deposition stress and subsequent temperature change. Also given are the specimen curvature and the strain energy release rate for interfacial debonding.

Language: Executable file only.

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D

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E

MAP_COMP_ESHCON

This program calculates either the electrical or the thermal conductivity of a composite material, using the Eshelby equivalent homogeneous inclusion method.

Language: Executable file only.

MAP_COMP_ESHCTE

This program calculates the thermal expansion coefficient (expansivity) of a composite material, using the Eshelby equivalent homogeneous inclusion method.

Language: Executable file only.

MAP_COMP_ESHELC

This program calculates the elastic constants of a composite material, using the Eshelby equivalent homogeneous inclusion method.

Language: Executable file only.

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F

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G

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H

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IJ

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K

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L

MAP_COMP_LAMSTI

This program calculates the elastic constants of a laminate (stack of plies), from the Young's modulus and Poisson ratio of fibre and matrix, the fibre volume fraction and the fibre orientation of each ply.

Language: Executable file only.

MAP_COMP_LAMSTR

This program calculates the stresses within a selected individual ply in a laminate (stack of plies), from the Young's modulus and Poisson ratio of fibre and matrix, the fibre volume fraction and the fibre orientation of each ply.

Language: Executable file only.

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M

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N

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O

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PQ

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R

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S

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T

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UVW

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XYZ

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