pylandjw
Petroleum
- Mar 30, 2007
- 2
Hi all,
We are constructing an FEA model of a structural steel frame. The members are custom built from steel plate. They are bolted together with custom built flanges also made of steel plate.
We have constructed a shell model in ANSYS using shell181 elements. We are having difficulty modeling the connections, and I am looking for suggestions on how to treat them.
Our first approach was to model both halves of the flange and connect the plates together with beam elements. There was no contact between the plates. This method produces very high stresses in the flanges and the nearby members. By bonding the plates together, the stresses decrease by 3 or four times, and this result matches more closely to simple hand calcs. But we will also need to get the loads on the bolts in the joint for a bolted joint type of calculation such as from Shigley and Mischke.
Any suggestions would be appreciated.
We are constructing an FEA model of a structural steel frame. The members are custom built from steel plate. They are bolted together with custom built flanges also made of steel plate.
We have constructed a shell model in ANSYS using shell181 elements. We are having difficulty modeling the connections, and I am looking for suggestions on how to treat them.
Our first approach was to model both halves of the flange and connect the plates together with beam elements. There was no contact between the plates. This method produces very high stresses in the flanges and the nearby members. By bonding the plates together, the stresses decrease by 3 or four times, and this result matches more closely to simple hand calcs. But we will also need to get the loads on the bolts in the joint for a bolted joint type of calculation such as from Shigley and Mischke.
Any suggestions would be appreciated.