Issue 74

O. Staroverov et alii, Fracture and Structural Integrity, 74 (2025) 358-372; DOI: 10.3221/IGF-ESIS.74.22

50 J or more, a breakthrough of the specimens occurs; with the reinforcement scheme [0/90] n , growth of the lamination area stops, while with the scheme [± 45] n , it continues to increase to E imp = 75 J.

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d Figure 2: The dependences of load on displacement and load on time for specimens with reinforcement schemes [0/90] n (a, c) and [±45] n (b, d), respectively

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