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...
Gespeichert in:
Veröffentlicht in: | Russian aeronautics 2014-07, Vol.57 (3), p.240-244 |
---|---|
Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
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 |