Issue 62

Yu. G. Matvienko et alii, Frattura ed Integrità Strutturale, 62 (2022) 541-560; DOI: 10.3221/IGF-ESIS.62.37

Corresponding circumferential strain   distributions are shown in Fig. 7.

a b Figure 5: Typical interferograms obtained at the same remote stress increments for the 2927th (a) and 3530th (b) loading cycles.

Figure 6: Distributions of the in-plane Cartesian displacement components u (1) and v (2) along the filled hole edge obtained after a surface crack appearance at 2927th (circular dots) and 3530th (triangular dots) loading cycles.

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