How the composite fails under load? - PowerPoint PPT Presentation

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How the composite fails under load?

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* Example of this mode is epoxy resin reinforced by carbon fibre. * Asssume a parallel coupling between fibres and matrix for stress parallel to axis 1. – PowerPoint PPT presentation

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Title: How the composite fails under load?


1
How the composite fails under load?
  • Consider the case in which a tensile stress
    acts parallel to the fibre (axis 1).
  •  
  • Fig. Fig.
  •  
  • Case 1 Ef lt Em
  •  
  • The mode of failure depend on Ef and Em.
  •  
  • Mode (1) is brittle fibres inductile matrix.
  • Mode (2) is dectile fibres in brittle matrix.
  •  

2
  • Example of this mode is epoxy resin reinforced
    by carbon fibre.
  • Asssume a parallel coupling between fibres and
    matrix for stress parallel to axis 1.
  • Also assume that fibres and matrix in the
    composite are to fail independently, at the
    same stresses and strains as when tensile tests
    are carried out on the pure material.
  •  
  • As strain is increased, a point is reached
    around Ef where fibre begin to break, and their
    contribution to the total stress falls to zero.

3
  • The second step depends on ?f (1) at low ?f
  •  
  • There is sufficient matrix to carry the tensile
    load even after all fibre have fialed.
  • And
  • The total stress at strain E1 is, from now on,
    Just the contribution of the matrix alone
  • (1-?f) ?m
  •  
  • Finally (with further straining)
  •  
  • The composite fails when the matrix which
    contain brokken fibres fails at E1 Em.

4
For high ?f
  • When the fibres break there is insufficient
    matrix to maintain the same stress
  •  
  • Thus the point of failure of the fibres then
    marks the failure of the composite also
  •  
  • In this case the stress just prior to failure
    is the sum of ?f?f and (1- ?f ) ?m
  •  
  • where ?m ?m (Ef). The stress carried by the
    matrix at the failure strain of the fibres.

5
? Summary
  • Low ?f ?1 (1 - ?f ) ?m (2.26a)
  • high ?f ?1 ?f?f (1- ?f) ?m (2.26b)

6
How to calculate the minimum volume fraction of
reinforcement.
  • Equations (2.26) give two estimates for ?1 as
    shown in the figure
  •  
  •  
  • Fig.
  •  
  •  
  • Except at vary low fibre fractions tensile
    strength is dominated by the contribution
  • from the fibres. ?1 ? ?f?f
  • Thus
  • A minimum fibre fraction is required before
    the fibre exert a strengthening effect at all.
  •  
  • Lower values of ?2 will result is weakening
    the matrix and must be avoided.
  • Therefore
  • ?fmin is a critical parameter.
  • ?fmin is obtained by equating ---- with
    ---- from equation (2.26b)
  •  

7
Example 6.
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12
Thank You
  • See You Next Lecture
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