Prediction of size effects in notched laminates using continuum damage mechanics
By Pedro P. Camanho, P. Maimí, C. Dávila. 2007
538 citations recorded by the source corpus.
Subfields: Building and Construction, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/b19eae6c5f33e2b2470f873fc2e94b3c91be8e92
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In Building and Construction
In Mechanics of Materials
Citations in the corpus
- Micro-mechanical analysis of the in situ effect in polymer composite laminates (2014, methodology): “The interlaminar properties of the IM7/8552 carbon-epoxy composite laminate [39] are used to model the interfaces between the intermediate 90◦ lamina and the adjacent homogenised ±θ◦ plies.”
- A procedure for superposing linear cohesive laws to represent multiple damage mechanisms in the fracture of composites (2009, methodology): “The longitudinal strengthof T300/913 was not available so the strength of a typical graphite/epoxy material was used: σc = 2,326MPa ( Camanho et al. 2007 ).”
- Size effects on the tensile and compressive failure of notched composite laminates (2013, result): “While the effect of the size on the strength of composite laminates with open holes, where increasing the size of specimens with constant width-to-diameter ratio decreases the strength, is well-know since the seventies [1], recent experiments [2] and analysis models [2–4] not only shed new light int”
- Measurement of resistance curves in the longitudinal failure of composites using digital image correlation (2010, unknown): “The elastic properties of IM7-8552, measured in a previous investigation [18], are shown in Table 1.”
- On cohesive element parameters and delamination modelling (2019, unknown): “Reference Material Simulation In-plane strength Yt / Sl (MPa) Interface strength / (MPa) Kp (N/mm(3)) Turon [45] AS4/PEEK DT 80/100 10(6) Harper [20] HTA6376/C DT 30/60 10(5) Soto [21] T300/977-2 DT 60/80 10(6) Dávila [75] IM6/3501-6 DT 61/68 Hallett [61] IM7/8552 OHT 60/90 60/90 Higuchi [37]; Caman”