faromic80
Structural
- Feb 14, 2008
- 80
I have some more questions about trusses and decided to start another thread because the one I started the other day is a little off topic. I have attached a scan of some questions I have on a truss I am analyzing. I got these shop drawings and have to verify everything works.
From what I understand, truss members have only axial loads, but this is not the case here. In the attachment I show the model i used for hand calcs: simply supported truss. Then I show the model with the existing columns coming up the sides. The top and bottom chords are attached to the existing columns at the sides. I also attached the RISA output for the top and bottom chords. The bottom chord has moment and NO axial loads?? The (2) C10x15.3 channels can't handle that moment. I'm thinking this is because of the connection to the existing columns? the top chord has both moment and large axial forces in it and I can't understand why? because of the distributed load on the top chord?
Also, the two center diagonal M15 and 16 have no axial force in them?
I don't exactly understand the splice connection at the top chord. I don't understand why the the two plates are welded on the the larger splice plate...is this for out of plane buckling reinforcement?
You can also see in the RISA model at the intersection of M8 and M9 the members don't coincide with the center of the top chord (see truss shop dwg) how can I model this in RISA?
As for the model I think it's pretty accurate because my hand calcs for the joint forces is within +-10 kips (attached)
From what I understand, truss members have only axial loads, but this is not the case here. In the attachment I show the model i used for hand calcs: simply supported truss. Then I show the model with the existing columns coming up the sides. The top and bottom chords are attached to the existing columns at the sides. I also attached the RISA output for the top and bottom chords. The bottom chord has moment and NO axial loads?? The (2) C10x15.3 channels can't handle that moment. I'm thinking this is because of the connection to the existing columns? the top chord has both moment and large axial forces in it and I can't understand why? because of the distributed load on the top chord?
Also, the two center diagonal M15 and 16 have no axial force in them?
I don't exactly understand the splice connection at the top chord. I don't understand why the the two plates are welded on the the larger splice plate...is this for out of plane buckling reinforcement?
You can also see in the RISA model at the intersection of M8 and M9 the members don't coincide with the center of the top chord (see truss shop dwg) how can I model this in RISA?
As for the model I think it's pretty accurate because my hand calcs for the joint forces is within +-10 kips (attached)