The Load Sequence Effect on Composite Laminates under Fatigue Loading
碩士 === 國立成功大學 === 航空太空工程學系 === 88 === Through non-destructive measurements, the cumulative damage of composite laminates subjected to fatigue loading can be evaluated. These can be done by measuring the reduction of stiffness and/or modulus. A Stiffness degradation model has been proposed and proved...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2000
|
| Online Access: | http://ndltd.ncl.edu.tw/handle/64617149165165582332 |