TY - JOUR
T1 - Effect of number of fatigue cycles on fatigue data
T2 - CFRP (prepreg and wet-layup)
AU - Banks-Sills, Leslie
AU - Choron, Tomer
AU - Simon, Ido
N1 - Publisher Copyright:
© 2023 The Authors. Fatigue & Fracture of Engineering Materials & Structures published by John Wiley & Sons Ltd.
PY - 2024/3
Y1 - 2024/3
N2 - In carrying out fatigue delamination propagation tests to assess the propagation rate versus a function of the energy release rate, the question arises as to the necessary number of cycles required to properly characterize the behavior. Tests were performed elsewhere on two different carbon/epoxy, multidirectional woven composite laminates containing a delamination using constant amplitude cycling by means of displacement control for various cycle ratios. The aim was to carry out the tests for (Formula presented.) cycles. Most specimens complied with this requirement. In this study, the fatigue data are analyzed including the first (Formula presented.) cycles, the first (Formula presented.) cycles, the first (Formula presented.) cycles, and (Formula presented.) cycles. It was seen that although the delamination length versus the cycle number could be quite similar between different cycle ranges, the Paris relation constants could be significantly different. It is suggested to carry out tests for as many cycles as possible.
AB - In carrying out fatigue delamination propagation tests to assess the propagation rate versus a function of the energy release rate, the question arises as to the necessary number of cycles required to properly characterize the behavior. Tests were performed elsewhere on two different carbon/epoxy, multidirectional woven composite laminates containing a delamination using constant amplitude cycling by means of displacement control for various cycle ratios. The aim was to carry out the tests for (Formula presented.) cycles. Most specimens complied with this requirement. In this study, the fatigue data are analyzed including the first (Formula presented.) cycles, the first (Formula presented.) cycles, the first (Formula presented.) cycles, and (Formula presented.) cycles. It was seen that although the delamination length versus the cycle number could be quite similar between different cycle ranges, the Paris relation constants could be significantly different. It is suggested to carry out tests for as many cycles as possible.
KW - constant amplitude
KW - energy release rate
KW - fatigue cycles
KW - fatigue delamination growth rate
KW - fiber reinforced polymer composites
UR - http://www.scopus.com/inward/record.url?scp=85180189649&partnerID=8YFLogxK
U2 - 10.1111/ffe.14199
DO - 10.1111/ffe.14199
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AN - SCOPUS:85180189649
SN - 8756-758X
VL - 47
SP - 833
EP - 848
JO - Fatigue and Fracture of Engineering Materials and Structures
JF - Fatigue and Fracture of Engineering Materials and Structures
IS - 3
ER -