A Beginner's Guide to the Steel Construction Manual, 14^th ed.

Chapter 8 - Bending Members

© 2006, 2007, 2008, 2011 T. Bartlett Quimby

Section 8.2.5

Compression Flange Local Buckling Limit State

Last Revised: 07/30/2011

Local buckling of the compression flange (FLB) occurs when the width/thickness ratio of the plate elements is high. The general concept was discussed in some detail in the notes on plate buckling. The specific application to flexural members is found in SCM Chapter F. Using SCM Table User Note F1.1 as a reference, one or the other of FLB appears in SCM F3, F4, F5, F6, F7, and F9.

Note that there are a limited number of rolled sections which have problems with FLB and WLB. The SCM user notes in F2, F3, and F6 point out the sections that are likely to have problems with WLB and FLB for a given range of F_y. As F_y increases, more sections become non-compact and slender, thus invoking WLB and FLB limits on strength.

The Limit State

The basic limit state follows the standard form.  The statement of the limit states and the associated reduction factor and factor of safety are given here:

The values of M_u and M_a are the LRFD and ASD factored loads, respectively, applied to the flexural member. 

In this case M_n is the nominal FLB limited flexural strength of the member. Since this is a buckling phenomenon, limits need to be found for the three strength regions: plastic, inelastic buckling, and elastic buckling as shown in Figure 8.2.1.5.

The General Form

The general form of the FLB limit state follows the typical buckling curve. The slenderness parameter used is width/thickness ratio (b/t) as specified in SCM B4.

The limits of the buckling regions are specified by the terms l_p (the limit of the plastic region) and l_r (the limit of the inelastic buckling region). Hence:

• if l = b/t < l_p then the plastic strength, M_p, controls and FLB does not occur
• if l_p < l = b/t < l_r then inelastic FLB occurs
• if l_r < l = b/t then elastic FLB occurs

Figure 8.2.5.1 illustrates the concept.

Figure 8.2.5.1
General FLB Strength
Click on image for larger view

Both l_p and l_r are computed using the appropriate cases and equations from SCM Table B4.1.

M_p

• SCM F3:  M_p = F_yZ_x 
• SCM F4:  M_p = R_pcM_yc = R_pcF_yS_xc, as found in SCM F4.1.  
  • R_pc is computed using SCM Eq. F4-9.
• SCM F5:  Stresses are used instead of moments. F_y takes the place of M_p (extracted from SCM equation F5-8) in the general form of the equation for the inelastic buckling region. M_p becomes R_pgF_yS_xc (SCM equation F5-7)
• SCM F6:  M_py = min (F_yZ_y, 1.6F_yS_y), (SCM eq F6-1)
• SCM F7: M_px = F_yZ, (SCM eq F7-1)

M_r

The moment at the interface of the elastic and inelastic ranges, M_r, is found embedded in the linear interpolation function found in several of the specification sections used to compute the strength in the inelastic buckling range.

• SCM F3:  M_r = 0.7F_yS_x (extracted from SCM equation F3-1)
• SCM F4:  M_r = F_LS_xc (extracted from SCM equation F4-12)
• SCM F5:  Stress is used instead of moments. F_r takes the place of M_r (F_r = 0.3F_y, extracted from SCM equation F5-8) in the general form of the equation for the inelastic buckling region.
  • While not used in the equations of SCM F5, M_r = R_pgF_rS_xc.
• SCM F6: M_r = 0.7F_yS_y (extracted from SCM equation F6-2)
• SCM F7:  The general form of the inelastic buckling equation is not used (though the ones used are still linear with b/t) so computing M_r is not useful.
• SCM F9: M_r = 0.7F_yS_x (extracted from SCM equation F9-6)

Plastic Range

As noted above, when l < l_p FLB does not happen. Consequently in the plastic range, M_n equals M_p.

In-elastic Buckling Range

• SCM F3, F4, & F6:  A linear interpolating function is used to compute M_n in the in-elastic buckling range. This resulting value is compared with M_p to find the final M_n.

The equation can be written as:

M_n = min [(M_p - (M_p - M_r)*(l - l_p)/(l_r - l_p)), M_p]

• SCM F5:  A similar linear interpolation function is used (SCM equation F5-8):

M_n = F_crR_pgS_xc = min [(F_y - 0.3F_y (l - l_p)/(l_r - l_p)), F_y] R_pgS_xc

• SCM F7: (SCM equation F7-2)

• For SCM F9: (SCM equation F9-6, adapted)

M_n = min [(M_p - (M_p - M_r)*(l - l_p)/(l_r - l_p)), 1.6M_y]

Elastic Buckling Range

The nominal moment capacity, M_n, in the elastic range is found by computing the elastic moment that creates the critical buckling stress, F_cr, in the compression flange.

M_n = min[F_crS_xc, M_p]

A modified Euler type function is used to the compute the critical buckling stress, F_cr.

• SCM F3, F4, & F5: (SCM equations F3-2, F4-14, F5-9)

• SCM F7: (SCM equation F7-3)

M_n = F_yS_e

• where S_e is an effective section modulus which is determined using an effective flange width computed with SCM equation F7-4.

• SCM F9: (SCM equation F9-7, with l = b_f/2t_f)

Download a summary of FLB equations here.

The following spreadsheet example computes the major axis flexural capacity, M_nx, including FLB effects, for a typical W section.  The input values are in the grey shaded cells and the result in the yellow highlighted cell.

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