| タイトル | The Effects of Fiber Surface Modification and Thermal Aging on Composite Toughness and Its Measurement |
| 本文（外部サイト） | http://hdl.handle.net/2060/19960012186 |
| 著者（英） | Bowles, Kenneth J.; Papadopolous, Demetrios S.; Madhukar, Madhu; Mccorkle, Linda; Inghram, Linda |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1995-12-01 |
| 言語 | eng |
| 内容記述 | A detailed experimental study was conducted to establish the structure-property relationships between elevated temperature aging and fiber-matrix bonding, Mode 2 interlaminar fracture toughness, and failure modes of carbon fiber/PMR-15 composites. The fiber-matrix adhesion was varied by using carbon fibers with different surface treatments. Short beam shear tests were used to quantify the interfacial shear strength afforded by the use of the different fiber surface treatments. The results of the short beam shear tests showed that, for times up to 1000 hr, the aging process caused no changes in the bulk of the three composite materials that would degrade the shear properties of the material. Comparisons between the interlaminar shear strengths (ILSS) measured by the short beam shear tests and the GIIC test results, as measured by the ENF test, indicated that the differences in the surface treatments significantly affected the fracture properties while the effect of the aging process was probably limited to changes at the starter crack tip. The fracture properties changed due to a shift in the fracture from an interfacial failure to a failure within the matrix when the fiber was changed from AU-4 to AS-4 or AS-4G. There appears to be an effect of the fiber/matrix bonding on the thermo-oxidative stability of the composites that were tested. The low bonding afforded by the AU 1 fiber resulted in weight losses about twice those experienced by the AS 1 reinforced composites, the ones with the best TOS. |
| NASA分類 | COMPOSITE MATERIALS |
| レポートNO | 96N18423
NASA-TM-106765
NAS 1.15:106765
E-9816
NIPS-96-08132 |
| 権利 | No Copyright |
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