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Nondestructive testing of defects in adhesive joints

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Figure 3: Von-mises stress distribution show<strong>in</strong>g over a section <strong>of</strong> structure modelled with 30 % short glass fibre filled<br />

polycarbonate. Maximum stress <strong>of</strong> 48 MPa is obta<strong>in</strong>ed <strong>in</strong> the lower h<strong>in</strong>ge section shown by the circle.<br />

Figure 4: Von-mises stress distribution show<strong>in</strong>g over a section <strong>of</strong> structure modelled with 40% Unidirectional glass fibre<br />

re<strong>in</strong>forced Epoxy. Maximum stress <strong>of</strong> 58 MPa is obta<strong>in</strong>ed <strong>in</strong> the lower h<strong>in</strong>ge section shown by the circle.<br />

Figure 5: Von-mises stress distribution show<strong>in</strong>g over a section <strong>of</strong> structure modelled with 40% Unidirectional carbon fibre<br />

re<strong>in</strong>forced Epoxy. Maximum stress <strong>of</strong> 320 MPa is obta<strong>in</strong>ed <strong>in</strong> the lower h<strong>in</strong>ge section shown by the circle.<br />

Figure 6: Total Vector displacement distribution show<strong>in</strong>g over a section <strong>of</strong> structure modelled with 30 % short glass fibre filled<br />

polycarbonate . Max. displacement <strong>of</strong> 35 mm at the lower end <strong>of</strong> the component as shown by ellipse.

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