blogan
Aerospace
- Mar 7, 2007
- 11
I am modeling a fairly simple composite box beam that has a balanced, symmetric layup (-45,45,0,45,-45). I have tried modeling the beam using two approaches because I can't find any examples of how to model a laminate.
The first approach I tried was to define one Section ("ply layup") with five plies in the correct stacking sequence. I then created one Section Assignment using "ply layup" and selected all surfaces of the beam.
The second approach I tried was to define three Sections ("layer -45", "layer 45", "layer 0") with one ply each. I then created five Section Assignments using each of the three Sections in the correct stacking sequence.
Otherwise the models were exactly the same but when I view results they are very different. I am new to ABAQUS but not new to FEA software. Please tell me why these approaches give different results and which one is correct.
PLEASE HELP
Thanks
P.S. An explanation of how to correctly model a layup would be extremely helpful. For example, what is the correct way to model ply drops, lap joints, stagered plies, etc?
The first approach I tried was to define one Section ("ply layup") with five plies in the correct stacking sequence. I then created one Section Assignment using "ply layup" and selected all surfaces of the beam.
The second approach I tried was to define three Sections ("layer -45", "layer 45", "layer 0") with one ply each. I then created five Section Assignments using each of the three Sections in the correct stacking sequence.
Otherwise the models were exactly the same but when I view results they are very different. I am new to ABAQUS but not new to FEA software. Please tell me why these approaches give different results and which one is correct.
PLEASE HELP
Thanks
P.S. An explanation of how to correctly model a layup would be extremely helpful. For example, what is the correct way to model ply drops, lap joints, stagered plies, etc?