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Direct Strength Prediction of Cold-Formed Steel Beam-Columns . Y. Shifferaw , B.W. Schafer Research Progress Report to MBMA February 2012. Origins of a different approach. Steel beam-column design (hot-rolled and cold-formed) traditionally follows an interaction equation approach.
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Direct Strength Prediction of Cold-Formed Steel Beam-Columns Y. Shifferaw, B.W. Schafer Research Progress Report to MBMA February 2012
Origins of a different approach • Steel beam-column design (hot-rolled and cold-formed) traditionally follows an interaction equation approach. • The origins of which can be traced back to the much beloved engineering solution to stress in a beam:
Origins of a different approach (cont.) • First yield (for section symmetric about axis of bending) follows this linear interaction:but, basically nothing else! • In CFS design it is presumed that first yield may be replaced by nominal capacity: For CFS recall that these capacities are determined from relatively complex calculations, that we may summarize as.. Py and My might behave, but what about all these “cr”’s, local, distortional and global buckling??
Traditional CFS interaction approach(locally slender example) Py Pn Pcrl Mn My Mcrl
Let’s fire up my favorite tool and explore what stability does under the more complex demands of a beam column
Reference stress 0.25Py,0.75My Applied as reference loads 1/3 P/M ratio… 0.25Py 0.75My
Comparing stability solutions Stability does not follow the linear interaction, can be better, worse or same…
P,Mxx,Mzz all at the same time! +0.25MZZy -0.25MZZy
Origins of a different approach (cont.) • Conclusion from this little FSM study is that elastic buckling is dependent on cross-section and on applied demands (P, Mx, Mz) in a nonlinear fashion. • Cross-section stability analysis which picks up this dependency is available. • Standard interaction approach is limited and can not take advantage of situations when stability is favorable, instead always assumes a worst case linear reduction…
Traditional CFS interaction approach(locally slender example) Revisited Py Pn Pcrl Mn My Mcrl
CFS interaction(locally slender example) unsymmetric bending axis.. Py Pn Pcrl Mn My Mcrl
CFS interaction(locally slender example) unsymmetric bending axis.. Py Pn Pcrl Mn My Mcrl How to generalize formulation to take advantage of this, is the research!
Research • Proposal goes back to 2008, solicited from AISI • 2011 MBMA partnered with AISI to help fund the first year of the work • Research is now underway • Long term potential is greater than CFS, but with DSM in AISI-S100 it is the logical starting place
Industry assistance • ADTEK (Jeffrey Klaiman), • NUCON1(Rick Haws, Anwar Merchant & BaoPham), • MESCO (Harley Davidson), • BUTLER (Al Harroldand FredericoBueno) • ALPINE (Tamil Samiappan and Bill Babich). and • MBMA (Lee Shoemaker) • AISI (Jay Larson) 1. R.I.P.
Selecting industry relevant beam-columnsCFS Framing Model buildings from • Devco (CFS-NEES) • Adtek • Nucon CFS-NEES building
Focus on Secondary (CFS) members Like eave strut.. and of course purlins and girts
Identifying key beam-columns… M only P+M d=1.079” t=0.068” 0.25 0.68 0.25 0.68 0.94 0.36 0.36 Combined axial and bending stress index 0.14 0.14
Continuous Eave strut design example LC30=1.0D+0.750L+0.750WPA2 W( 1.0D+0.750L) P=( f(0.750WPA2))
Preliminary formulation Demands set the Pr/Mr ratio of interest, which is the slope of this line! Py Pn by Pcrl bn bcrl Mn My Mcrl
Preliminary formulation (2) For local buckling of a stub section, P or M simply replaced by b! y
Selecting industry relevant beam-columnsCFS Framing Model buildings from • Devco (CFS-NEES) • Adtek • Nucon CFS-NEES building
Focusing on most efficient sections Pn/A All CFS framing members Most efficient Mn/A
Selection based on predicted limit states Axial local Bending dist. Axial dist Bending local Axial local Bending yield Axial dist Bending yield Local only! Distortional only! Focus is here in the limited year one work, expansion to more complicated cases in years 2 and 3 if funded Color indicates an efficient section
Modeling • Nonlinear shell FE models of imperfect CFS member • End displacements over desired P, Mx, My • Boundary conditions and lengths to isolate local and distortional buckling • Preliminary models completed with success
Potential! Local DSM vs minor axis strength bounds for C