Data underlying the article: Early fatigue damage accumulation of CFRP Cross-Ply laminates considering size and stress level effects
doi: 10.4121/21222371
Ply-block size and stress level effect on accumulation of transverse cracks and delamination are investigated during early fatigue life of CFRP laminates. Tension-tension fatigue tests under different stress levels were performed for two cross-ply configurations. Edge observation with digital cameras, digital image correlation and acoustic emission were employed for in-situ damage monitoring. Transverse cracks were dominant for [0/902]s laminates with almost non-existent delamination, while different interactive levels between both damage mechanisms occurred for [02/904]s laminates. Poisson’s ratio identifies whether early fatigue damage is dominant by transverse cracks or involves delamination. Cumulative AE energy is a helpful indicator of crack density.
- 2022-09-29 first online, published, posted
DATA
- 3,685 bytesMD5:
f3bf73ffa2e0e214e5da631ab3a455f6
README.txt - 59,601 bytesMD5:
dd1bd33b4736d642d502394b35ef6a47
Figure 10.xlsx - 60,822 bytesMD5:
bd3d654e2c896672329e401961123aae
Figure 11.xlsx - 71,066 bytesMD5:
96b991776cc9e0b945d7063a3a632c2d
Figure 12(a).xlsx - 85,182 bytesMD5:
8555b64d054aef3cd68f8c2f57920290
Figure 12(b).xlsx - 95,156 bytesMD5:
3d706460283a9378b8e6ed9e62339aa9
Figure 13.xlsx - 107,624 bytesMD5:
ad2083917889025c802b7d014ef09652
Figure 14(a).xlsx - 102,289 bytesMD5:
c6c76a460c0b2f7b3c3d15ce7930ed34
Figure 14(b).xlsx - 52,297 bytesMD5:
c02ee822f03a9e1b5b1bee7b14f7169a
Figure 15.xlsx - 88,756 bytesMD5:
3542cd6399e30a7c1eed59647a90d095
Figure 2.xlsx - 84,535 bytesMD5:
faf46f03c2361b2f3a3369db3fbe081a
Figure 3.xlsx - 88,301 bytesMD5:
94fc7844b1f5de797c7f907fcff6b610
Figure 5.xlsx - 94,726 bytesMD5:
01363dca646d18d14f4421fd4d6c20d2
Figure 6.xlsx - 71,722 bytesMD5:
35b938a80db7f8b84d3f7ae9e9c2e365
Figure 8.xlsx - 150,462 bytesMD5:
5875ef52a2230940b19df2b7ed002c22
Figure 9.xlsx -
download all files (zip)
1,216,224 bytes unzipped