Issue 53

A. Moulgada et alii, Frattura ed Integrità Strutturale, 53 (2020) 187-201; DOI: 10.3221/IGF-ESIS.53.16

Figure 7: Variation of the maximum normal stresses  xx according to the various loadings

Shear stresses  xy For the different loads, we compare the different tangential stresses for the unrepaired plate and after its repair by composite patch, which is Boron/Epoxy and Carbon/Epoxy; we have obtained the following results:

« Load 20 MPa»

« Load 40 MPa»

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