Abstract
Automatic system has been developed to determine stress intensity factors in cracked panels. The system is based on small-size displacement gauges. A computer provides remote control and enables to perform measurements in real time, to calculate stress-intensity factors and applied loads. The following D16T sheet alloy specimens have been investigated: a cracked plate, a stiffened plate with a crack under a central stringer and between stringers.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 72-77 |
| Number of pages | 6 |
| Journal | Fiziko-Khimicheskaya Mekhanika Materialov |
| Volume | 29 |
| Issue number | 2 |
| State | Published - Mar 1993 |
| Externally published | Yes |
ASJC Scopus subject areas
- Mechanics of Materials