| タイトル | Fracture Mechanics for Composites: State of the Art and Challenges |
| 本文（外部サイト） | http://hdl.handle.net/2060/20080014103 |
| 著者（英） | Krueger, Ronald; Krueger, Ronald |
| 著者所属（英） | National Inst. of Aerospace Associates |
| 発行日 | 2006-05-31 |
| 言語 | eng |
| 内容記述 | Interlaminar fracture mechanics has proven useful for characterizing the onset of delaminations in composites and has been used with limited success primarily to investigate onset in fracture toughness specimens and laboratory size coupon type specimens. Future acceptance of the methodology by industry and certification authorities however, requires the successful demonstration of the methodology on the structural level. In this paper, the state-of-the-art in fracture toughness characterization, and interlaminar fracture mechanics analysis tools are described. To demonstrate the application on the structural level, a panel was selected which is reinforced with stringers. Full implementation of interlaminar fracture mechanics in design however remains a challenge and requires a continuing development effort of codes to calculate energy release rates and advancements in delamination onset and growth criteria under mixed mode conditions. |
| NASA分類 | Composite Materials |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
