作者: Maria Pia Falaschetti , Francesco Rondina , Lorenzo Donati , Enrico Troiani
DOI: 10.1016/J.PROMFG.2020.04.119
关键词: Composite number 、 Epoxy 、 Composite material 、 Shell (structure) 、 Materials science 、 Failure mode and effects analysis 、 Bar (music) 、 Finite element method 、 Material properties 、 Compression (physics)
摘要: Abstract In this paper a sensitivity study of FEM model representing carbon/epoxy composite material tested in Combined Loading Compression (CLC) is presented and the results are compared to experimental results. The present aims simulate failure materials when subjected compression crush loading conditions. This required as first step Building-Block Approach towards full-scale modelling complex structures. part work, laminate panel was manufactured with carbon unidirectional prepreg (Deltapreg UTS-300-DT120-37EF) cross-ply, balanced symmetric stacking sequence, cured autoclave at 120°C 5 bar for 90 min. A number six samples, extracted from panel, were following ASTM D6641/D6641M-16. Numerical simulations have been implemented by means commercial software, ESI-VPS PAM CRASH. Boundary conditions, specimens’ dimensions properties emulated real test performed on critical simulation parameters: effect mesh size shell surfaces sequence initially investigated. Furthermore, specimen mode inspected application TIED links between plies. data comparison provided references testing scale-up Approach.