Last Friday, I got a call from a wood truss supplier. Apparently, when they pre-fabbed the walls (2' o.c studs), they were built such that the studs did not line up with the trusses above (also 2' o.c.). Thus the trusses have the potential to land on the top plates as point loads (2000 lb approx) at midspan between studs. The truss guys wanted me to evaluate wheather or not this condition was acceptable.
I would like to solicit comments and recommendations on the method of analysis for the capacity of stud wall top plates.
Here are my thoughts and concerns:
1. For bending stress, I think that the top plate should be analyzed as two separate members with no consideration given to the lamination between them. Thus, the bending capacity would be twice the capacity of a single 2x6 used flat.
2. I wonder if I should even use both of the plates for capacity. Since it is possible for one of the plates to be spliced between any two studs, perhaps I should only count on the bending resistance of one plate.
3. For shear check, I do not believe that the lack of lamination between the plates reduces the capacity. I assume the the shear capacity of two stacked 2x6 would be the same as one piece 3.0" x 5.25" (Using the allowable stress values corresponding to the 2x6's of course).
4. Is it valid to use both top plates for shear capacity even though there may be a splice break in one of them?
When I checked the shear in this way, I found that the capicity is pretty damn small. Sample Calc:
-Double 2x6 Plate
-Ch = 2.0 (Not very conservative)
-fv = 70 psi (#1/#2 SPF)
-Duration factor (1.15)
Vr = 1.15 x 0.667 x 3.0 x 5.25 x 70 psi = 1690 lb
At 50 PSF total roof loading and 2' truss spacing, that amounts to the reaction from only a 34' simply supported truss. I commonly encounter trusses that span more than 34'. What is especially disconcerting to me is that since this limit is based on the shear caused by a single point load, it doesn't really help the situation to reduce the spacing of the studs.
Is there something that I am missing here? Is there some analytical way to account for the help that the top plates may get from the sheathing? Any advice that anyone has for me on this topic would be greatly appreciated. Thanks in advance for your efforts.
Adam
I would like to solicit comments and recommendations on the method of analysis for the capacity of stud wall top plates.
Here are my thoughts and concerns:
1. For bending stress, I think that the top plate should be analyzed as two separate members with no consideration given to the lamination between them. Thus, the bending capacity would be twice the capacity of a single 2x6 used flat.
2. I wonder if I should even use both of the plates for capacity. Since it is possible for one of the plates to be spliced between any two studs, perhaps I should only count on the bending resistance of one plate.
3. For shear check, I do not believe that the lack of lamination between the plates reduces the capacity. I assume the the shear capacity of two stacked 2x6 would be the same as one piece 3.0" x 5.25" (Using the allowable stress values corresponding to the 2x6's of course).
4. Is it valid to use both top plates for shear capacity even though there may be a splice break in one of them?
When I checked the shear in this way, I found that the capicity is pretty damn small. Sample Calc:
-Double 2x6 Plate
-Ch = 2.0 (Not very conservative)
-fv = 70 psi (#1/#2 SPF)
-Duration factor (1.15)
Vr = 1.15 x 0.667 x 3.0 x 5.25 x 70 psi = 1690 lb
At 50 PSF total roof loading and 2' truss spacing, that amounts to the reaction from only a 34' simply supported truss. I commonly encounter trusses that span more than 34'. What is especially disconcerting to me is that since this limit is based on the shear caused by a single point load, it doesn't really help the situation to reduce the spacing of the studs.
Is there something that I am missing here? Is there some analytical way to account for the help that the top plates may get from the sheathing? Any advice that anyone has for me on this topic would be greatly appreciated. Thanks in advance for your efforts.
Adam