| タイトル | Micromechanics Fatigue Damage Analysis Modeling for Fabric Reinforced Ceramic Matrix Composites |
| 本文（外部サイト） | http://hdl.handle.net/2060/20130014831 |
| 著者（英） | Xue, D.; Shi, Y.; Min, J. B. |
| 発行日 | 2013-05-01 |
| 言語 | eng |
| 内容記述 | A micromechanics analysis modeling method was developed to analyze the damage progression and fatigue failure of fabric reinforced composite structures, especially for the brittle ceramic matrix material composites. A repeating unit cell concept of fabric reinforced composites was used to represent the global composite structure. The thermal and mechanical properties of the repeating unit cell were considered as the same as those of the global composite structure. The three-phase micromechanics, the shear-lag, and the continuum fracture mechanics models were integrated with a statistical model in the repeating unit cell to predict the progressive damages and fatigue life of the composite structures. The global structure failure was defined as the loss of loading capability of the repeating unit cell, which depends on the stiffness reduction due to material slice failures and nonlinear material properties in the repeating unit cell. The present methodology is demonstrated with the analysis results evaluated through the experimental test performed with carbon fiber reinforced silicon carbide matrix plain weave composite specimens. |
| NASA分類 | Space Transportation and Safety; Structural Mechanics; Aircraft Design, Testing and Performance |
| レポートNO | NASA/TM-2013-217870
E-18663 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/84580 |
