TY - JOUR
T1 - Testing of Brazilian Disk Specimens with a Delamination between a Transversely Isotropic and a Tetragonal Composite Ply
AU - Mega, Mor
AU - Banks-Sills, Leslie
N1 - Publisher Copyright:
© 2018 The Authors.
PY - 2018
Y1 - 2018
N2 - Fracture toughness tests using the Brazilian disk specimen (BD) were carried out to determine the toughness properties of a delamination between two fiber reinforced composite plies. The upper ply is a transversely isotropic UD fabric with fibers oriented in the 0-direction and the lower ply is a tetragonal plain balanced weave with fibers oriented in the +45°/-45°-directions. The composite is manufactured as a wet-layup. With the BD specimen, mixed mode combinations are achieved by changing the loading angle ω, between the load line and the delamination. Eight specimens were tested at four loading angles, two for each angle. Based on the test results, finite element (FE) analyses were carried out in conjunction with two methods, the three-dimensional conservative M-integral and displacement extrapolation (DE) to obtain the stress intensity factors along the delamination front for each specimen resulting from mechanical loads, as well as residual stresses. The two methods were used in order to validate the results. Both methods were extended for this specific interface and made use of the first term of the asymptotic solution of the displacement field. The stress intensity factors were superposed, and the critical interface energy release rates and phase angles were calculated and plotted.
AB - Fracture toughness tests using the Brazilian disk specimen (BD) were carried out to determine the toughness properties of a delamination between two fiber reinforced composite plies. The upper ply is a transversely isotropic UD fabric with fibers oriented in the 0-direction and the lower ply is a tetragonal plain balanced weave with fibers oriented in the +45°/-45°-directions. The composite is manufactured as a wet-layup. With the BD specimen, mixed mode combinations are achieved by changing the loading angle ω, between the load line and the delamination. Eight specimens were tested at four loading angles, two for each angle. Based on the test results, finite element (FE) analyses were carried out in conjunction with two methods, the three-dimensional conservative M-integral and displacement extrapolation (DE) to obtain the stress intensity factors along the delamination front for each specimen resulting from mechanical loads, as well as residual stresses. The two methods were used in order to validate the results. Both methods were extended for this specific interface and made use of the first term of the asymptotic solution of the displacement field. The stress intensity factors were superposed, and the critical interface energy release rates and phase angles were calculated and plotted.
KW - Delamination
KW - Fracture toughness
KW - Interface energy release rate
KW - Multidirectional composite
KW - Stress intensity factors
UR - http://www.scopus.com/inward/record.url?scp=85064719472&partnerID=8YFLogxK
U2 - 10.1016/j.prostr.2018.12.021
DO - 10.1016/j.prostr.2018.12.021
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AN - SCOPUS:85064719472
SN - 2452-3216
VL - 13
SP - 123
EP - 130
JO - Procedia Structural Integrity
JF - Procedia Structural Integrity
T2 - 22nd European Conference on Fracture, ECF 2018
Y2 - 25 August 2018 through 26 August 2018
ER -