Mohammad-Abazari / FEM_CFRP_hollowCylinders

FEM_CFRP_hollowCylinders

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This Matlab program homogenizes and solves for the material response of cylindrical hollow composites consisting of helically oriented fiber reinfoced plies under pure bending loads.

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The program was built as a part of a Master thesis at Chalmers University of Technology, Department of Applied Physics, 2015.

Title of thesis: "Improved material performance in floorball sticks - Implementation of the Finite Element Method for helically fiber-oriented laminae in cylindrical hollow composites" Author: Mats Lindström, mats.at.lindstrom@gmail.com

Remark: This program is based on a supplement to the paper "Matlab-Implementation of the Finite Element Method in Elasticity" by J. Alberty, C. Carstensen, S. A. Funken, and R. Klose.

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main.m is a Matlab script generating:

  • The mesh of a hollow cylindrical coordinate system from coordGenerator.m,
  • Homogenized material properties using effCompMatrix.m, where cylCompMat.m transforms the local coordinate system to its global equivalent
  • A FEM simulation using FEMcylinder.m, where
    • stima.m assembles the element stiffness matrix,
    • f.m describes volume forces such as gravitational forces,
    • g.m describes surface (traction) forces,
    • u_d.m describes Dirichlet conditions
  • Results visualized using show.m

A stack of different ply configurations can be assembled, simulated and visualized by running stackGenerator.m, stackSim.m and plotLaminateStacking.m

%%%%%%%%%%%%%%%%%%%%%%%%%% Functions %%%%%%%%%%%%%%%%%%%%%%%%%%

Functions for single configurations

% Coordinates and triangulation of hollow cylinder [coordinates,elements,neumann,dirichlet] = coordGenerator(meshDim)

% Effective material compliance matrix of homogenized material S = effCompMatrix(phi,meshDim,E,nu,G)

% Local ply coordinate system to global S = cylCompMat(phi, E, nu, G)

% Displacement via FEM u = FEMcylinder(S,coordinates,elements,neumann,dirichlet,meshDim,force)

% Element stiffness matrix assembly stima = stima(vertices,S)

% Volume forces volforce = f(x)

% Surface forces sforce = g(x,normal,dA,meshDim,force)

% Dirichlet conditions [W,M] = u_d(x)

% Visualize triangulation show(dirichlet,neumann,coordinates)

Special functions for multiple configurations

% Set of stacks consisting of different angles, number of plies, etc. stacks = stackGenerator(nAngles,nPlies,scenario)

% Run FEM for different stacks laminate = stackSim(stacks,E,nu,G,meshDim,coordinates,elements,dirichlet,neumann,force)

% Plot obtained results from stack simulations SCRIPT: plotLaminateStacking.m

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FEM_CFRP_hollowCylinders

License:MIT License


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