Abstract
The high-cycle fatigue characteristics, especially the initiation and propagation of edge delamination, were investigated with quasi-isotropic carbon fiber reinforced plastic (CFRP) laminates with a stacking sequence of [45/0/-45/90]S. To investigate the influence that transverse cracks have on the initiation and propagation of edge delamination, two types of specimens are used. One was a specimen where transverse cracks were arbitrarily introduced by static tensile loading before conducting the fatigue tests. The other was an undamaged specimen as new. As a result, it was found that the single transverse crack introduced before the fatigue test did not seriously affect the initiation of edge delamination. Moreover, the difference of the fatigue damage growth behavior depending on the applied stress level was observed. Under the test conditions of low-applied stress level and high-cyclic loadings, it was observed that the edge delamination grew before, or simultaneously with, the transverse crack propagation.
| Original language | English |
|---|---|
| Title of host publication | ICCM International Conferences on Composite Materials |
| Publication status | Published - 2007 |
| Event | 16th International Conference on Composite Materials, ICCM-16 - "A Giant Step Towards Environmental Awareness: From Green Composites to Aerospace" - Kyoto Duration: 2007 Jul 8 → 2007 Jul 13 |
Other
| Other | 16th International Conference on Composite Materials, ICCM-16 - "A Giant Step Towards Environmental Awareness: From Green Composites to Aerospace" |
|---|---|
| City | Kyoto |
| Period | 07/7/8 → 07/7/13 |
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Keywords
- Cfrp laminates
- Composites
- Delamination
- Free-edge effects
- High-cycle fatigue
- Transverse crack
ASJC Scopus subject areas
- Engineering(all)
- Ceramics and Composites
Cite this
Interaction between transverse cracks and edge delamination considering free-edge effects in composite laminates. / Hosoi, Atsushi; Yagi, Shinako; Nagata, Keiichi; Kawada, Hiroyuki.
ICCM International Conferences on Composite Materials. 2007.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Interaction between transverse cracks and edge delamination considering free-edge effects in composite laminates
AU - Hosoi, Atsushi
AU - Yagi, Shinako
AU - Nagata, Keiichi
AU - Kawada, Hiroyuki
PY - 2007
Y1 - 2007
N2 - The high-cycle fatigue characteristics, especially the initiation and propagation of edge delamination, were investigated with quasi-isotropic carbon fiber reinforced plastic (CFRP) laminates with a stacking sequence of [45/0/-45/90]S. To investigate the influence that transverse cracks have on the initiation and propagation of edge delamination, two types of specimens are used. One was a specimen where transverse cracks were arbitrarily introduced by static tensile loading before conducting the fatigue tests. The other was an undamaged specimen as new. As a result, it was found that the single transverse crack introduced before the fatigue test did not seriously affect the initiation of edge delamination. Moreover, the difference of the fatigue damage growth behavior depending on the applied stress level was observed. Under the test conditions of low-applied stress level and high-cyclic loadings, it was observed that the edge delamination grew before, or simultaneously with, the transverse crack propagation.
AB - The high-cycle fatigue characteristics, especially the initiation and propagation of edge delamination, were investigated with quasi-isotropic carbon fiber reinforced plastic (CFRP) laminates with a stacking sequence of [45/0/-45/90]S. To investigate the influence that transverse cracks have on the initiation and propagation of edge delamination, two types of specimens are used. One was a specimen where transverse cracks were arbitrarily introduced by static tensile loading before conducting the fatigue tests. The other was an undamaged specimen as new. As a result, it was found that the single transverse crack introduced before the fatigue test did not seriously affect the initiation of edge delamination. Moreover, the difference of the fatigue damage growth behavior depending on the applied stress level was observed. Under the test conditions of low-applied stress level and high-cyclic loadings, it was observed that the edge delamination grew before, or simultaneously with, the transverse crack propagation.
KW - Cfrp laminates
KW - Composites
KW - Delamination
KW - Free-edge effects
KW - High-cycle fatigue
KW - Transverse crack
UR - http://www.scopus.com/inward/record.url?scp=79960033851&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=79960033851&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:79960033851
SN - 9784931136052
BT - ICCM International Conferences on Composite Materials
ER -