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X. Bi et al.
smallest. In general, the size of delamination damage is smaller than that of in-plane
damage (mainly in-plane matrix damage).
13.5.2 Analysis of the Influence of Embedded Delamination
on Skin-Stringer Debonding
Figure 13.14 shows the effect of different size embedded defects on skin-stringer
debonding. It can be studied that the delamination propagation law is basically consistent. For the middle truss with embedded defects, delamination mainly extends from
the right half to the left, and the left side begins to gradually occur when the right
side is almost completely layered.
Fig. 13.14 Effect of embedded delamination on skin-stringer debonding
X. Bi et al.
smallest. In general, the size of delamination damage is smaller than that of in-plane
damage (mainly in-plane matrix damage).
13.5.2 Analysis of the Influence of Embedded Delamination
on Skin-Stringer Debonding
Figure 13.14 shows the effect of different size embedded defects on skin-stringer
debonding. It can be studied that the delamination propagation law is basically consistent. For the middle truss with embedded defects, delamination mainly extends from
the right half to the left, and the left side begins to gradually occur when the right
side is almost completely layered.
Fig. 13.14 Effect of embedded delamination on skin-stringer debonding