Abstract
The effect of the stress ratio on fatigue characteristics in the out-of-plane direction of thick carbon fiber reinforced plastic (CFRP) laminates with toughened interlaminar layers was evaluated. The spool shaped specimens cut out the unidirectional thick CFRP laminates, which pile up 88 plies of the prepreg with toughened interlaminar layer, T800S/3900-2B, were used. The fatigue tests were conducted under the stress ratios of R = 0.1 and -1 to evaluate the effect of the stress ratio. As the results of the fatigue tests, the fatigue life of the specimens at R = -1 was shorter than that at R = 0.1. It was found that the fatigue properties of the CFRP laminates in the out-of-plane direction are affected by the stress amplitude from the experimental results. In addition, the fatigue life under the different stress ratio can be evaluated equivalently using the Walker model which can consider the mean stress effect.
| Original language | English |
|---|---|
| Publication status | Published - 2015 Jan 1 |
| Event | 20th International Conference on Composite Materials, ICCM 2015 - Copenhagen, Denmark Duration: 2015 Jul 19 → 2015 Jul 24 |
Other
| Other | 20th International Conference on Composite Materials, ICCM 2015 |
|---|---|
| Country | Denmark |
| City | Copenhagen |
| Period | 15/7/19 → 15/7/24 |
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Keywords
- Fatigue
- Out-of-plane
- Stress ratio
- Thick CFRP laminates
- Toughened interlaminar layers
ASJC Scopus subject areas
- Engineering(all)
- Ceramics and Composites
Cite this
Effect of stress ratio on fatigue characteristics in the out-of-plane direction of thick CFRP laminates with toughened interlaminar layers. / Hosoi, Atsushi; Sakuma, Shigeyoshi; Seki, Sen; Fujita, Yuzo; Taketa, Ichiro; Kawada, Hiroyuki.
2015. Paper presented at 20th International Conference on Composite Materials, ICCM 2015, Copenhagen, Denmark.Research output: Contribution to conference › Paper
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TY - CONF
T1 - Effect of stress ratio on fatigue characteristics in the out-of-plane direction of thick CFRP laminates with toughened interlaminar layers
AU - Hosoi, Atsushi
AU - Sakuma, Shigeyoshi
AU - Seki, Sen
AU - Fujita, Yuzo
AU - Taketa, Ichiro
AU - Kawada, Hiroyuki
PY - 2015/1/1
Y1 - 2015/1/1
N2 - The effect of the stress ratio on fatigue characteristics in the out-of-plane direction of thick carbon fiber reinforced plastic (CFRP) laminates with toughened interlaminar layers was evaluated. The spool shaped specimens cut out the unidirectional thick CFRP laminates, which pile up 88 plies of the prepreg with toughened interlaminar layer, T800S/3900-2B, were used. The fatigue tests were conducted under the stress ratios of R = 0.1 and -1 to evaluate the effect of the stress ratio. As the results of the fatigue tests, the fatigue life of the specimens at R = -1 was shorter than that at R = 0.1. It was found that the fatigue properties of the CFRP laminates in the out-of-plane direction are affected by the stress amplitude from the experimental results. In addition, the fatigue life under the different stress ratio can be evaluated equivalently using the Walker model which can consider the mean stress effect.
AB - The effect of the stress ratio on fatigue characteristics in the out-of-plane direction of thick carbon fiber reinforced plastic (CFRP) laminates with toughened interlaminar layers was evaluated. The spool shaped specimens cut out the unidirectional thick CFRP laminates, which pile up 88 plies of the prepreg with toughened interlaminar layer, T800S/3900-2B, were used. The fatigue tests were conducted under the stress ratios of R = 0.1 and -1 to evaluate the effect of the stress ratio. As the results of the fatigue tests, the fatigue life of the specimens at R = -1 was shorter than that at R = 0.1. It was found that the fatigue properties of the CFRP laminates in the out-of-plane direction are affected by the stress amplitude from the experimental results. In addition, the fatigue life under the different stress ratio can be evaluated equivalently using the Walker model which can consider the mean stress effect.
KW - Fatigue
KW - Out-of-plane
KW - Stress ratio
KW - Thick CFRP laminates
KW - Toughened interlaminar layers
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M3 - Paper
AN - SCOPUS:85018604210
ER -