Data for: Low velocity impact resistance of thin and toughened carbon fibre reinforced epoxy

Version v2: 
Added tiff-image stacks

Version v1:
The data is supplementary to the publication "Low velocity impact resistance of thin and toughened carbon fibre reinforced epoxy", DOI: 10.1016/j.compscitech.2022.109362 as well as to the dissertation: "Morphology and Fracture of Block Copolymer and Core-Shell Rubber Particle Modified Epoxies and their Carbon Fibre Reinforced Composites", urn: urn:nbn:de:hbz:386-kluedo-63437

Key words: Polymer-matrix composites (PMCs), Impact behaviour, Low velocity impact, Barely visible impact damage, Damage tolerance, X-ray computed tomography, Fractography, Carbon fibre reinforced composite (CFRP)

The data set is a collection of TXRM data of several low energy impact damages in CFRP specimens. The data was acquired via XCT (X-Ray Computed Tomography).

Material details:

• Carbon fibre reinforced composite
• Thickness: ~ 1.65mm
• Matrix polymer: Epoxy-based (DGEBA): Sika CR144 + Anhydride curing agent (Huntsman Aradur917) + 1-Methylimidazole
• Carfon-fibre fabric: ECC Carbon fabric Style 763, based on Toho Tenax HTA40 E13, 140g/m²
• Layup: 13 layers, stacking sequence (45/-45/45/-45/90/0/90)s, (15% 0°/23% 90°/62% ± 45°) 
• the average carbon fibre volume content was 52.5 ± 1.8 vol.-%
• cured ply-thickness: 126.1 μm
• Impact energies: 1J, 3J, 7J, 9J, 13J
• manufactured via autoclaving

The reasearch received funding from the German Academic Exchange Service (DAAD) within the funding program “Kurzstipendien fuer Doktoranden” (grant number: 57438025).