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MATS1101 - Engineering Materials and Chemistry - T3 2025

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If the matrix and reinforcement materials are the same, select one composite out of the three shown that you would expect to have the highest toughness.

image of composites

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Given the derivations you have done, and the moduli calculated for the same material under isostrain conditions and isostress conditions in Questions 1 & 2, which of the following diagrams do you think would give the best stiffness?

formulae

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From this isostrain equation you can see that the matrix, which has a low modulus, acts to decrease the composite modulus. What then is the principal role of the matrix in fibre-reinforced composites?

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A composite consisting of aligned glass fibres in a polyester matrix is loaded in a direction parallel to the reinforcing fibres. If there is 30 vol% fibres, modulus of the fibres is 70 GPa and modulus of polyester is 4.4 GPa, determine the fraction of the total composite load carried by the fibres.

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A composite containing carbon fibres in epoxy resin is loaded in a direction perpendicular to the reinforcing fibres. If there is 55 vol% fibres, modulus of the carbon fibres is 340 GPa and modulus of epoxy is 3.2 GPa, determine the modulus of the composite. Use this equation to calculate the modulus of the composite:

 

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A composite containing carbon fibres in epoxy resin is loaded in a direction parallel to the reinforcing fibres. If there is 45 vol% fibres, modulus of the carbon fibres is 380 GPa and modulus of epoxy is 3.0 GPa, determine the modulus of the composite. Use this equation to calculate the modulus of the composite:

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Given the derivations you have done, and the moduli calculated for the same material under isostrain conditions and isostress conditions in Questions 1 & 2, which of the following diagrams do you think would give the best stiffness?

formulae

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If the matrix and reinforcement materials are the same, select one composite out of the three shown that you would expect to have the highest toughness.

image of composites

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0%
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You have calculated the composite modulus for carbon fibres in epoxy resin, both parallel and perpendicular to the reinforcing fibres. Explain the difference in values between the two.

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From this isostrain equation you can see that the matrix, which has a low modulus, acts to decrease the composite modulus. What then is the principal role of the matrix in fibre-reinforced composites?

Formulae

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100%
0%
0%
0%
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