LockeBT
Structural
- May 9, 2021
- 55
In almost every single structural analysis books I've read, truss analysis is performed under the conditions of "ideal trusses":
1) Distributed forces along the member are neglected and forces are summed up and applied as point loads at the nodes/connections.
2) Members are only designed for axial loads (tension or compression).
3) Nodes/connections are considered to be pinned.
I'm ok with the 3rd condition since it's more conservative than assuming that there are some fixity at the nodes/connections. No worries there.
However, let's focus on the 1st and 2nd conditions. It's a bit counter-intuitive for me given how that's not a conservative approach. A member subjected to combined flexural and axial loading (mainly compression) has reduced capacity because it has to satisfy the unity equation. Even if the member is fully braced along its compression edge I still have such reduced capacity that I will need to upsize said member compared to the it being designed for axial load alone.
I have always analyzed the truss as a whole (using the ideal truss method) to figure out the axial forces in each member. Then go back and apply distributed loadings such as wind, dead and live loads on said members (especially the ones in compression) and check it for flexure + compression. It just makes more sense to me. And more often than not I end up using a larger member.
Does anyone else do this?
1) Distributed forces along the member are neglected and forces are summed up and applied as point loads at the nodes/connections.
2) Members are only designed for axial loads (tension or compression).
3) Nodes/connections are considered to be pinned.
I'm ok with the 3rd condition since it's more conservative than assuming that there are some fixity at the nodes/connections. No worries there.
However, let's focus on the 1st and 2nd conditions. It's a bit counter-intuitive for me given how that's not a conservative approach. A member subjected to combined flexural and axial loading (mainly compression) has reduced capacity because it has to satisfy the unity equation. Even if the member is fully braced along its compression edge I still have such reduced capacity that I will need to upsize said member compared to the it being designed for axial load alone.
I have always analyzed the truss as a whole (using the ideal truss method) to figure out the axial forces in each member. Then go back and apply distributed loadings such as wind, dead and live loads on said members (especially the ones in compression) and check it for flexure + compression. It just makes more sense to me. And more often than not I end up using a larger member.
Does anyone else do this?