I have modelled the plate using 11 ply layer in composite layup manager in ABAQUS including the Aluminum and glass fiber layers. Al/0/90/0/90/Al/90/0/90/0/Al is the layup. I am using Aluminum with combination of two failure model Johnson cook and ductile damage. And glass fiber with USDFLD code and engineering constant properties. Larger cutout is incorporated then in this layup and smaller ones too. But in the end in postbuckling and buckling behavior showing buckling loads are larger of large cutout than smaller cutout (CIRCULAR CUTOUT).
Plates are square
Can you share your model (6.13 is comfortable), so that I can help you
This is the model sir. i have modelled it using continuum shell too and solid plate with interactions. Tell me what model you need if you find any solution to the problem. PB is for postbuckling too you can use fortran file if needed
- Badges
- Science topic
- Similar topics
- Physical Sciences
- Materials Science
- Plating