This must be one big tower to require bracing like that. FWIR, the staggered Leg bracing was used after a lot full scale testing by SAE from somewhere in Europe, Spain I think. I'm not sure if you can use the 1.2 factor in this case. The SAE tests were done on leg (corner post) members where there were 2 planes of support from the 2 tower faces where the stagger was used. In your case, the stagger is in one plane and out of plane buckling is the big question. If member P7 is the corner post leg and this drawing is the longitudinal face lacing pattern, then member P7T is in the same plane as P7 and P7L. If I am reading the drawing correctly, then P7T has staggered bracing in this plane but where is it braced for out of plane buckling?
If you use the latest version of PLS-CADD software, you can model all the redundants in the TOWER model and the nonlinear analysis will show where this bracing pattern will buckle. I would model this panel in PLS-TOWER with all members and use the 1.2 factor and apply a big compression load on leg P7 and a little wind perpendicular to the face using ASCE-74-2009M so you get wind on all the redundants and lacing members, then I would run a NL analysis and see if the panel is stable. Members P7T and P7L will be beam members.
I guess it depends if you want to gamble that the staggered bracing factors can be used and pick smaller members for P7T, or you can be conservative and assume P7T buckles out of plane where it is braced.
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