LSPSCAT
Structural
- Dec 19, 2007
- 123
For a situation with grillage beam assembly with several beams sitting cross wise on a carrier beam I have used rigid links connected between the centroid of the shapes to model the behavior. At the node that ties to the carrier beam I have released all moments as my initial attempt without releasing the moments in the rigid link introduced too much stiffness. The beams are simply bolted to each other, flange to flange. Does anyone have any additional insight to model this behavior?
At the top of the grillage there are plates welded continuously to the upper member. For this case I have used rigid links with out any releases to model the composite action. Seems to give overall accurate behavior although this method requires some work outside of Risa to check the composite section properties of the stiffened plate composed of wide flanges welded to the underside of the plate.
At the top of the grillage there are plates welded continuously to the upper member. For this case I have used rigid links with out any releases to model the composite action. Seems to give overall accurate behavior although this method requires some work outside of Risa to check the composite section properties of the stiffened plate composed of wide flanges welded to the underside of the plate.