| タイトル | A model for the progressive failure of laminated composite structural components |
| 著者（英） | Lo, D. C.; Allen, D. H. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1991-01-01
1991 |
| 言語 | eng |
| 内容記述 | Laminated continuous fiber polymeric composites are capable of sustaining substantial load induced microstructural damage prior to component failure. Because this damage eventually leads to catastrophic failure, it is essential to capture the mechanics of progressive damage in any cogent life prediction model. For the past several years the authors have been developing one solution approach to this problem. In this approach the mechanics of matrix cracking and delamination are accounted for via locally averaged internal variables which account for the kinematics of microcracking. Damage progression is predicted by using phenomenologically based damage evolution laws which depend on the load history. The result is a nonlinear and path dependent constitutive model which has previously been implemented to a finite element computer code for analysis of structural components. Using an appropriate failure model, this algorithm can be used to predict component life. In this paper the model will be utilized to demonstrate the ability to predict the load path dependence of the damage and stresses in plates subjected to fatigue loading. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 93A31286 |
| 権利 | Copyright |
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