BMart006
Structural
- Mar 20, 2017
- 61
I am personally not a fan of codes without commentaries, and I'm currently working with two of them (CMAA70 and MH27.1). Both of them feature an equation for the maximum compression stress (from flexure) for a single web monorail crane as Stress Allowed (ksi) = 12000 / ((Lbd)/Af) < 0.6Fy. Lb is the unbraced length of the top flange and Af is the compression flange area. FYI monorails are usually not doubly symmetric or of the same material as the top flange and web. That being said, this looks like a buckling formula of sorts, but there is no commentary in either code to provide the origin. Anyone have any thoughts on where this comes from or if it is really sufficient for an unsymmetrical section with two different Fys?