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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2012
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Article
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Fig 7
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Research Article
Experimental and Numerical Failure Analysis of Adhesive Composite Joints
Figure 7
(a) Contour for evaluation of the
-integral. (b) Contour integral around the crack tip. (c) Finite element mesh pattern of around the crack-tip of DCB [
36
].
(a)
(b)
(c)