acga
Aerospace
- Apr 14, 2014
- 2
Hi everyone,
I'm currently working on a FEM model (Nastran) that due to geometrical reasons must have both shell and solid elements.
I must create several bolted connections between shell-solid and my intention is purely to transfer loads between them. Stress distribution around the bolted area is not important.
My first approach was to connect a node from the shell and another from the solid element through and RBE2 element, where the dependant and independant grids depend on the load path (in some cases it's from shell-to-solid and in others the otherway around). However, with this approach bending moment is not transferred from shell-to-solid and so I think results may not be accurate.
Is there any other method to effectively transfer load from shell-to-solid and vice-versa?
Thanks!
acga
I'm currently working on a FEM model (Nastran) that due to geometrical reasons must have both shell and solid elements.
I must create several bolted connections between shell-solid and my intention is purely to transfer loads between them. Stress distribution around the bolted area is not important.
My first approach was to connect a node from the shell and another from the solid element through and RBE2 element, where the dependant and independant grids depend on the load path (in some cases it's from shell-to-solid and in others the otherway around). However, with this approach bending moment is not transferred from shell-to-solid and so I think results may not be accurate.
Is there any other method to effectively transfer load from shell-to-solid and vice-versa?
Thanks!
acga