jayrod12
Structural
- Mar 8, 2011
- 6,265
Hey everyone.
I have this steel roof truss comprised of double angles for all members with a 10' bay spacing for the bottom chord and verticals at the intermediate 5' marks for the top chords. This truss was designed and constructed in the late 60's under Canadian design standards.
I've checked a few of the components and it appears as though the original designer neglected combined action for the design of the top chord members. As far as I know your top chord must be supported at max 24" in order for you to neglect combined action or you must provide sufficient argument that the roof deck can transfer the load to the panel points.
When I run the existing members under the original loading (and using the applicable codes from the day for both loading determination and strength determination) for combined action they fail. Am I missing some provision?
I've used a slenderness of 0.9L/r where L is the panel length (5') and r of the 6x4x3/8" double angles (1.93 in) and the steel is 44ksi yield so I used 24.75ksi for allowable axial stress and 26.5ksi for allowable bending stress. Do these seem correct?
Granted it is not all of the members failing this way just the odd top chord member (I haven't got to checking the webs yet).
Would you consider continuous beam conditions for the top chord when analyzing for the moment? Something like wl^2/12?
I have this steel roof truss comprised of double angles for all members with a 10' bay spacing for the bottom chord and verticals at the intermediate 5' marks for the top chords. This truss was designed and constructed in the late 60's under Canadian design standards.
I've checked a few of the components and it appears as though the original designer neglected combined action for the design of the top chord members. As far as I know your top chord must be supported at max 24" in order for you to neglect combined action or you must provide sufficient argument that the roof deck can transfer the load to the panel points.
When I run the existing members under the original loading (and using the applicable codes from the day for both loading determination and strength determination) for combined action they fail. Am I missing some provision?
I've used a slenderness of 0.9L/r where L is the panel length (5') and r of the 6x4x3/8" double angles (1.93 in) and the steel is 44ksi yield so I used 24.75ksi for allowable axial stress and 26.5ksi for allowable bending stress. Do these seem correct?
Granted it is not all of the members failing this way just the odd top chord member (I haven't got to checking the webs yet).
Would you consider continuous beam conditions for the top chord when analyzing for the moment? Something like wl^2/12?