Fracture mechanics analysis of cylindrical panels with non-through cracks

This paper considers the fracture mechanics analysis in ANSYS for cylindrical panels with semielliptical non-through surface cracks. The results of calculating the fracture mechanics parameters along the defect front are presented. A universal formula for determining the stress intensity factor valu...

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Veröffentlicht in:Russian aeronautics 2014-07, Vol.57 (3), p.240-244
Hauptverfasser: Glushkov, S. V., Skvortsov, Yu. V.
Format: Artikel
Sprache:eng
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Zusammenfassung:This paper considers the fracture mechanics analysis in ANSYS for cylindrical panels with semielliptical non-through surface cracks. The results of calculating the fracture mechanics parameters along the defect front are presented. A universal formula for determining the stress intensity factor value at the representative points of the front line is proposed.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799814030040