Issue 50

O. Mouhat et alii, Frattura ed Integrità Strutturale, 50 (2019) 126-140; DOI: 10.3221/IGF-ESIS.50.12

(d) Von-Mises stress with a Layup sequence (45/-45/90/0) s; Composites with EG skin and CFC stiffener

(e) Von-Mises stress with a Layup sequence (60/-30/90/0) s; Composites with EG skin and CFC stiffener

(f) Von-Mises stress with a Layup sequence (90/0/90/0) s; Composites with EG skin and CFC stiffener Figure 7 : The Von-mises stresses at different composite materials and ply orientations of the panel with 4 Straight stiffeners.

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