Comparison between two and three parameters of fatigue crack growth models in airframe structures
Comparison of two and three parameters models of fatigue crack growth is discussed. For calculation of failure probability, the Monte Carlo (MC) method is used. The number of MC trials was 60. Multiple site fatigue damage specimens corroded to 5% to 6% average thickness loss and non‐corroded specim...
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Vilnius Gediminas Technical University
2005-06-01
|
| Series: | Aviation |
| Subjects: | |
| Online Access: | https://journals.vgtu.lt/index.php/Aviation/article/view/7411 |