Transcript Slide 1
Provisional ballot: Direct Strength Method for CFS compression members with holes Cris Moen and Ben Schafer AISI COS Meeting February 2009 DSM Holes (3+ years ago…) Pn = f (Py, Pcre, Pcrd, Pcrl)? Does f stay the same? Gross or net, or some combination? Explicitly model hole(s)? Accuracy? Efficiency? Identification? Just these modes? DSM Holes (today) Pn = f (Py, Pcre, Pcrd, Pcrl)? Column strength limited to Pynet DSM curves applicable when elastic buckling controls, changes needed though in inelastic regime Suite of approximate methods now available, “Local hole” buckling modes can affect strength DSM Holes (today) Consider three DSM options: Option 1 - Replace Py with Pynet everywhere Assumes net section exists along full length of column, conservative approach, easiest to implement Option 2 - Cap Pnl and Pnd at Pynet Places net section strength limit on existing DSM curves, can be unconservative in some cases Option 3 - Cap and transition Pnl and Pnd Transition from elastic buckling regime to net section cap at “knee” of DSM design curves, most accurate method but also increases work for engineers DSM Holes (Option 1) 1.2.X.X Flexural, Torsional, or Flexural-Torsional Buckling The nominal axial strength [resistance], Pne, for flexural, torsional, or torsional buckling including the influence of hole(s) shall be calculated in acc with the following: Replace Py with Pynet everywhere (a) For cnet 1.5 2cnet Pne = 0.658 (b) For cnet > 1.5 Pynet 0.877 P Pne = 2 ynet cnet where cnet = Pynet Pcre Pynet = AnetFy Anet = Net area of section at the location of hole(s) DSM Holes (Option 1) 1.2.X.X Distortional Buckling The nominal axial strength [resistance], Pnd, for distortional buckling inclu influence of hole(s) shall be calculated in accordance with the following: (a) For dnet 0.561 Pnd = Py net Replace Py with Pynet everywhere (b) For dnet > 0.561 0.6 P P crd crd Pnd = 1 0.25 P Pynet ynet where dnet = Pynet Pcrd 0.6 Pynet Pynet = A value as given in Eq. 1.2.X-X Pcrd = Critical elastic local column buckling load inclu influence of hole(s) determined by analysis in accordance wit 1.1.2 DSM Holes (Option 1) 1 Existing DSM curve (no holes) 0.9 0.8 0.7 Pnd/P y 0.6 Replace Py with Pynet everywhere (Option 1) 0.5 0.4 0.3 0.2 Assumptions for this plot: Pynet=0.80Py 0.1 0 0 0.5 1 1.5 2 2.5 distortional slenderness, d or dnet 3 DSM Holes (Option 1) 1.4 Existing DSM curve 1.2 Ptest/P y 1 0.8 FE simulated test data, Pynet=0.80Py 0.6 0.4 0.2 0 0 0.5 1 1.5 2 2.5 3 distortional slenderness, d=(Py /P crd )0.5 3.5 4 DSM Holes (Option 2) 1.2.X.X Local Buckling The nominal axial strength [resistance], Pnl, for local buckling includ influence of holes shall be calculated in accordance with the following: (a) For l 0.776 Pnl = Pne Pynet Cap strength at Pynet (b) For l > 0.776 P Pnl = 1 0.15 crl Pne where l = Pne Pcrl 0.4 P crl Pne 0.4 Pne Pynet Pne = A value as defined in Section 1.2.X.X Pcrl = Critical elastic local column buckling load including the influ hole(s) determined by analysis in accordance with Section 1.1.2 Pynet = AnetFy DSM Holes (Option 2) 1.2.1.3 Distortional Buckling The nominal axial strength [resistance], Pnd, for distortional buckling i influence of holes shall be calculated in accordance with the following: (a) For d 0.561 Pnd = Py Pynet Cap strength at Pynet (b) For d > 0.561 0.6 0.6 Pcrd Pcrd Py Pynet Pnd = 1 0.25 Py Py where d = Py Pcrd Py = A value as given in Eq. 1.2.1-4 Pcrd = Critical elastic distortional column buckling load including t of hole(s) determined by analysis in accordance with Section DSM Holes (Option 2) 1.4 Existing DSM curve 1.2 DSM Holes Option 2, cap at Pynet 1 Ptest/P y (b) 0.8 FE simulated test data, Pynet=0.80Py 10% 0.6 0.4 For smaller holes ,data deviates more gradually from design curve 0.2 0 0 0.5 1 1.5 2 2.5 3 distortional slenderness, d=(Py /P crd )0.5 3.5 4 DSM Holes (Option 2) 1.4 Existing DSM curve 1.2 Ptest /P y 1 DSM Holes Option 2, cap at Pynet 0.8 FE simulated test data, Pynet=0.60Py 0.6 25% 0.4 0.2 0 0 0.5 1 1.5 2 2.5 3 distortional slenderness, d=(Py /P crd )0.5 3.5 4 DSM Holes (Option 3) 1.2.X.X Local Buckling The nominal axial strength [resistance], Pnl, for local buckling in influence of holes shall be calculated in accordance with the following: (a) For l l 1 Pnl = Pne Pynet Cap strength at Pynet (b) For l1 l l 2 Pynet Pl 2 l l1 Pnl = Pynet l 2 l1 (c) For l > l 2 Pcrl Pnl = 1 0.15 Pne where 0.4 P crl Pne 0.4 Pne Transition to Pynet DSM Holes (Option 3) 1.2.1.3 Distortional Buckling The nominal axial strength [resistance], Pnd, for distortional buc influence of holes shall be calculated in accordance with the followi (a) For d d 1 Pnd = Pynet Cap strength at Pynet (b) For d1 d d 2 Pynet Pd2 d Pnd = Pynet Transition d 2 d 1 (c) For d1 d d 2 0.6 0.6 P P Pnd = 1 0.25 crd crd Py Py Py where to Pynet DSM Holes (Option 3) 1 Existing DSM curve (no holes) 0.9 Transition to Pynet (Option 3) 0.8 0.7 Pd2/Py Pnd/P y 0.6 0.5 0.4 0.3 d1 0.2 Assumptions for this plot: Pynet=0.80Py 0.1 0 d2 0 0.5 1 1.5 2 distortional slenderness, d 2.5 3 DSM Holes (Option 3) 1.4 Existing DSM curve 1.2 Ptest /P y 1 DSM Holes Option 3, cap and transition at Pynet 0.8 FE simulated test data, Pynet=0.60Py 0.6 0.4 0.2 0 0 0.5 1 1.5 2 2.5 3 distortional slenderness, d=(Py /P crd )0.5 3.5 4 Experiments Method Option, Description Local-global interaction Distortional buckling # of # of tests Mean SD tests Mean SD f f 1 - Pynet everywhere 1.17 0.09 0.89 47 1.22 0.13 0.87 15 DSM 2 - Cap Pnl, Pnd Holes 3 - Trans. Pnd,Pnl all data Main within code limits Spec outside code limits 1.07 0.08 0.90 42 1.06 0.13 0.85 29 1.06 1.12 1.20 1.06 0.08 0.12 0.12 0.06 0.89 0.87 0.88 0.91 47 63 27 36 1.13 1.11 *---* *---* 0.10 0.05 *---* *---* 0.89 0.91 *---* *---* 26 15 *---* *---* Ortiz-Colberg (1981), Sivakumaran (1987), Miller and Peköz (1994), AbdelRahman (1997), Pu et al. (1999), Moen and Schafer (2008) - All lipped C-sections - 85% stub columns - hhole/h varies from 0.10 to 0.60 Simulations Method Option, Description Local-global interaction Distortional buckling # of # of tests Mean SD tests Mean SD f f 1 - Pynet everywhere 1.14 0.13 0.86 93 1.24 0.18 0.83 176 DSM 2 - Cap Pnl, Pnd Holes 3 - Trans. Pnd,Pnl all data Main within code limits Spec outside code limits 1.06 0.15 0.83 93 1.09 0.17 0.82 186 1.08 1.06 1.04 1.07 0.85 0.86 0.88 0.86 89 1.04 0.19 236 0.91* 0.08 24 *---* *---* 212 *---* *---* 0.79 0.88 *---* *---* 200 149 *---* *---* 0.14 0.13 0.10 0.13 - All lipped C-sections, variety of short and long columns - 35 of 99 SSMA cross-sections represented - hhole/h varies from 0.10 to 0.80 - hole spacing varies from 8 to 24 inches Conclusions Option 1 - Replace Py with Pynet everywhere • Conservative over all slenderness ranges • Easy to implement Option 2 - Cap Pnl and Pnd at Pynet • Can be unconservative at “knee” of design curve • Easy to implement Option 3 - Cap and transition Pnl and Pnd • Most consistent with observed data trends • Additional effort to implement, use Also worth mentioning • Once DSM Holes is approved, Main Spec distortional buckling design method can be replaced • Should we prequalify hole shapes, sizes in DSM Holes? • Simplified elastic buckling methods could be used to improve Main Spec… Plate buckling with holes – Section B2, B3, B4 Distortional buckling with holes – C3.4.1, C4.2 Euler buckling with holes – C3.1.2, C4.1 • Goal is to incorporate stiffened holes into DSM Holes next… DSM Holes (Option 3) 1.4 1. 1.2 1. Existing DSM curve (no holes) 1 nl P /P y 0.8 P /P nl y Transition to Pynet Pcre=100P yg (Option 3) Pynet=0.8Pyg Pl2/Py 0.6 0.4 l1 0 Pcre=100Py (stub column) Pynet=0.8Py 0 0.5 1 1.5 0. 0. l2 0.2 0. 2 2.5 local slenderness, =(P /P )0.5 ne cr l l 3 3.5 0. 4 DSM Holes (Option 3) 1.4 1.2 P /P nl y 1 0.8 0.6 0.4 mn) 3.5 Option 3 assumes no net section influence when Pynet≥Pnl (i.e. existing DSM curve and DSM Holes curve are the same when Pynet ≥ Pnl) Pcre=Py (long column) Pynet=0.8Py 0.2 4 0 0 0.5 1 1.5 2 2.5 local slenderness, =(P /P )0.5 ne cr l l 3 3.5 4