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About Crack Growth Simulation and Residual Strength Prediction in Airplane Fuselages
presumes that any damage initiated by fatigue, accident, or corrosion will be found before catastrophic failure. [138]. The safety of the aircraft heavily depends upon finding cracks before they reach a critical length. The occurrence of WFD, however, drastically reduces the residual strength or de
Detailed Information
| Author: | Unknown |
|---|---|
| Pages: | 189 |
| Language: | English |
| File Size: | 8.66 |
| Format: | |
| Price: | FREE |
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