TedEP
Structural
- Feb 3, 2011
- 15
I have an architecturally driven stair stringer design challenge. The stringer spans 2 flights of stairs and 3 landings, see attached sketch. As such, there are 4 "kinks" in the beam. I know that the beam has to be designed for the global moment WL*L/8, with full strength welds at the kinks to develop the member capacity.
What about the local affects at the kinks? I believe there needs to be a stiffener at the joint, designed for axial load. The axial load, C or T, is derived from breaking the flange forces down into components, see sketch.
Comments? Is it really this straight forward?
What about the local affects at the kinks? I believe there needs to be a stiffener at the joint, designed for axial load. The axial load, C or T, is derived from breaking the flange forces down into components, see sketch.
Comments? Is it really this straight forward?