serdardundar
Structural
- Oct 6, 2001
- 19
I have a wall panel with light gauge thin walled studs with 0.8cm^2 effective area and KLx =1m KLy=1m KLt=1m . It is used to support the load coming from several shelves (if uniform distribution is assumed 330kgf acting on stud). The panel and the shelves above it are moved several meters; somehow during this movement some eccentricity occured in the studs (i am pretty sure about this) i don't know the amount of eccentricity. Same load is acting on the shelf. If i want to reanalyse the situation. Should i only calculate the stress P/A+P*(delta)/Wy (the eccentricity is in the weak direction of the studs, studs are C shaped by the way)? If this is done, the studs would be O.K. up to 1.2cm of top deflection. But i know that this deflection will cause the studs buckle (i think lateral torsional buckling will occur) very earlier than the load that i have calculated for the no eccentricity case (620kgf with Fy=1900kgf/cm^2). I am pretty sure that the governing mode of failure will be the lateral torsional buckling whereas i include the effect of eccentricity only in max stress calculations. So the problem is how should i include the effect of this eccentricity in my stability calculations? What will be the knew buckling load? I remember from my Special Concepts of Structural Stability course, the solution passes through virtual work principles and there are some methods in book of Galambos. But what i wonder is how do the codes approach to the problem, is there some kind of a formula or a simplified method in the codes for handling this?