13-Solved Problem 4-6-How to Find the Available Flexural Strength?

Last Updated on September 14, 2026 by Maged kamel

A solved problem 4- 6: How to Find the Available Flexural Strength?

A solved problem 4-6 for lateral-torsional buckling when lb>Lp but<Lr.

From Prof. Alan Williams’s book, Structure Reference Manual, solved problem 4.6: A W16x40 Beam of grade 50 steel is laterally braced at 6 ft intervals. It is subjected to a uniform bending Moment with the Moment coefficient Cb = 1.0.

Determine the Beam’s available flexural strength. This graph represents the relation between Lb and the nominal Moment Mn; it has three zones based on the Value of bracing length Lb and its relation with Lp and Lr.   

Solved problem 4-6, for which the flexure strength is required.

Analysis for the given section by the LRFD design.

Solved Problem 4-6 is an analysis problem; the section is given with a Beam bracing distance Lb such that Lp < Lb < Lr for LRFD design. It falls in the second Zone of inelastic buckling; see the next slide for details.

How do we get the values of Lp and Lr?

We need to find both bracing lengths lp and Lr for the given W section, which we can obtain from Tables 1-1 and 3-2. From Table 1-1, we need ry to estimate Lp. For lr, we need sufficient data to determine it, as we will see next.

Determine the maximum unbraced length required for the section to reach its plastic Moment strength, Lp. The relevant equation for Lp is Lp = 300*ry/sqrt(Fy). We need to get these data from AISC Table 1-1. The LP Value is 5.55 feet. Our given bracing length is 6 feet, and the condition is that the bracing length is greater than Lp. Please refer to the slide image for more details.

Estimate the lp value from the formula:3000*ry/sqrt(Fy)

We need the following values from the Torsional properties: J, CW, and other properties((tf, Sx, rts, ho)), selected from Table 1-1.

The different parameters for estimating Lr

This is the equation for the Lr formula using equation F2-6.

The formula used to estimate the value of Lr.

This is the detailed reference equation number as presented in the AISC code.

The equation of Lr in terms of E, j, c Fy Sx, ho and rts.

This is the detailed estimation of Lr using the equation.Lr=15.9′.

The value of lr after estimation for W16x40

This is the limiting laterally unbraced length, L, from Table 3-2 for W16x48.

The value of Lr, from Table 3-2 for W16x40

For the given Lb, check whether Lb > Lp and Lb < Lr; then the section is not compact. The Value of φb*Mn is < φb*(Mpx), but φb*Mn > φb*(Mrx), where Mpx=Fy*Zx, while Mrx= (0.70*Fy*Sx).

Estimate φb*Zx*Fy for Lb and φb*Fy*Sx for  Lr. Estimate the Value of φb *BF.

The next picture explains the final φb*Mn= φb (Zx*Fy)- φb *BF*(Lr-Lb).
The available flexure strength is based on LRFD: φb*Mn = 269.50 ft-kips.  

The value of Mn from BF.

These are the values of φb*Mp and φb*Mr using Table 3-2.

Using table 3-2 to get the available strength or factored moments.

I have used an Excel plot to show the relation between Lb and φb*Mn.

Using excel graph to represent lb versus phi Mn.

The analysis for the given section is by ASD.

We will use Table 3-2 to get (1/ωb) Mp and (1/ωb) Mr. We also get Lp and Lr values for W16x40.
  The given bracing length, lb = 6 ft, is greater than Lp but less than Lr.

The section is not compact, the value of Mn/Ω is < (Mpx)/ Ωb, > (1/Ωb)*(Mrx)
Mpx=Fy*Zx, Mrx= (0.70*Fy*Sx).

The values of Mpx/ Ωb and (1/ Ωb )*Mrx from table 3-2.

Estimate (1/Ωb)*Zx*Fy for Lb and (1/Ωb)* 0.70*Fy*Sx for Lr.   
The final (1/Ωb)*Mn= (1/Ωb) (Zx*Fy)- (1/Ωb) *Bf *(Lr-Lb).The available flexural strength based on ASD is (1/ωb)*n = 179.00 ft-kips.

These are the detailed calculations for the ASD Moment Value using BF, as shown in the next slide image.

The allowable flexure strength based on the ASD design.

I have used an Excel plot to show the relationship between Lb and (1/Ωb)*Mn.

Excel graph between Lb and Mn/omega for the ASD design.

The PDF containing the data for this post is available for review and download via the button below.

This is a Link to the solved problem 4-5. Solved problem 4-5. Design a steel Beam: Lb less than Lp.

For the next post, A Solved problem 9-7: When Lb> Lr, what is flexural strength?

Here is the Link to Chapter 8, “Bending Members.” A Beginner’s Guide to the Steel Construction Manual, 14th ed.

Here is the Link to Chapter 8, “Bending Members.” A Beginner’s Guide to the Steel Construction Manual, 15th ed.

Here is the Link to Chapter 8, “Bending Members.” A Beginner’s Guide to the Steel Construction Manual, 16th ed.