書誌事項
- タイトル別名
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- Polymer Matrix Composites. Fracture Mechanism for Mode II Propagation of Delamination Fatigue Cracks in CF/PEEK Laminates.
- 1ホウコウ キョウカ CF PEEK セキソウバン ノ モード 2 ソウカン
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抄録
The effect of stress ratio on the near-threshold growth of delamination fatigue cracks was investigated with unidirectional CFRP laminates made from toughened thermoplastic matrix resin. Tests were carried out under mode II shear loading by using end notched flexure specimens with a special loading device. The crack growth behavior under different stress ratios indicated that the fatigue crack growth rate was well correlated to the stress intensity range near the threshold region. The fatigue crack growth resistance of CF/PEEK laminates was slightly higher than that of conventional CF/epoxy laminates. However, the increase of the fatigue crack growth resistance by toughening the matrix resin was smaller than that under mode I loading. The reason for this poor toughening effect was discussed based on fractographic observation. Comparison of the change of stress-ratio dependency and the relative fatigue threshold was made from brittle CF/epoxy laminates to toughened CF/PEEK laminates under both mode I and mode II loadings. The stress-ratio dependency and the relative threshold were expressed by unique functions of the fracture toughness of the same laminates under the same loading modes.
収録刊行物
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- 材料
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材料 46 (4), 366-373, 1997
公益社団法人 日本材料学会
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詳細情報 詳細情報について
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- CRID
- 1390282680368502656
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- NII論文ID
- 110002293275
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- NII書誌ID
- AN00096175
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- COI
- 1:CAS:528:DyaK2sXivVOqtrs%3D
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- ISSN
- 18807488
- 05145163
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- NDL書誌ID
- 4182690
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
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- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可