Semi-elliptical surface cracks, growing due to cyclic loading of plates, undergo significant shape change during the propagation process. An equation for predicting this shape variation for any combination of tension and bending loading is presented. These growing cracks change their shapes such tha
On some spacecraft fatigue-crack propagation problems
✍ Scribed by József Gedeon
- Publisher
- Elsevier Science
- Year
- 1985
- Tongue
- English
- Weight
- 375 KB
- Volume
- 12
- Category
- Article
- ISSN
- 0094-5765
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