41-Practice problem 5-6-1-What is the available strength for W12x65?

Last Updated on February 25, 2026 by Maged kamel

Practice problem 5-6-1-What is the available strength for W12x65?

Practice problem 5-6-1. A W12x65 is used as a supported, uniformly loaded beam with a span length of 50 feet and continuous lateral support. The yield stress, Fy, is 50 ksi. If the ratio of live load to dead load is 3, what is the available strength for W12x65, and determine the maximum total service load, in kips/ft, that can be supported? a. Use LRFD. b. Use ASD.

I will include only the LRFD design in this post. Practice problem 5-6-1 is from the Steel Design Handbook.

Check the local buckling parameters for W12x65.

For the given W12x65, with fy=50 ksi and continuous lateral support, we need to determine the local buckling parameters bf/2tf and h/tw to confirm whether the section is compact or non-compact.

Practice problem 5-6-1-What is the AVSILSBLE STRENGTH FOR w12X65?
Practice problem 5-6-1-What is the available strength for W12x65?

We checked Table 1-1 for W12x65 and found that the section has a symbol’ f’, indicating that W12x65 doesn’t conform to the local buckling parameters.

Table 1-1 for W12x65.

We obtain the data required to solve practice problem 5-6-1: the values bf/2tf = 9.52 and h/tw = 24.90. The plastic section modulus Zx = 96.80 inch^3, and the elastic section modulus = 87.90 inch^3.

Table 1-1 part 2 find bf/2tf nd h/tw for W12x65.

As a reminder, please find the local buckling parameters for W sections with Fy = 50 ksi. Based on item 10 in Table B4.1b, the flange λFp=0.38*sqrt(E/Fy), since we have E29000 ksi and the given Fy=50 ksi, then λFp=0.38*sqrt(29000/50)=9.15. λFr=1.0*sqrt(E/Fy)=1*sqrt(29000/50)=24.08.

Local buckling parameters based on Fy=50 ksi.

For the web compactness ratio, λwp = 3.76*sqrt (E/Fy), λWp = 3.76*sqrt (29000/50) = 90.55. λwr=5.70*sqrt(E/Fy)=5.70*sqrt(29000/50)=137.27

Since bf/2tf is bigger than λFp, the flange is noncompact; hence, W12x65 is a non-compact section.

Find the values for Mpx and 0.7*Fy*Sx for W12x65.

Practice problem 5-6-1.The Plastic moment value equals Fy*Zx, which equals 50*96.8 = 4840 inches. Kips. The term (0.7*Fy*Sx) value equals 0.7*50*87.90=3076.50 Inch. Kips. The first term corresponds to λFp=9.15; the second corresponds to λFr=24.08.

Find Mpx and 0.70*Fy*Sx for W12x65.

Practice problem-5-6-1-What is the available strength for W12x65 based on local buckling?

To find the available strength Mn for W12x65 based on local buckling, we plot the relationship between λF and Mn; Mn can equal 4749 in. Kips can be approximated to 396 Ft. For the available strength φ*Mn, multiply by 0.9; the final answer is 356 ft. kips. This is the answer for part a.

Find the values for φ*Mn for W12x65.

What are the non-compact W sections based on Fy=50 ksi?

The following slide, from the companion of The AISC steel construction Manual, volume 1-design examples, lists nine non-compact W sections starting from W21x48 and ending with W6x8.50. The %centage reduction of the nominal moment is included for each W section.

List of Non compact W sections via AISC design examples data.

Create an Excel sheet for non-compact W sections with Fy = 50 ksi.

In the Excel sheet for non-compact W sections based on Fy=50 ksi, I have sorted the W sections with bf/2tf> 9.15 using an Excel sheet quoted from AISC W sections V15; the result is 10 W sections. Please refer to the next slide for more details.

An excel sheet for non compact W sections.

Adjustment in the Lp distance based on Mn.

The bracing Length Lp, which is equal to 10.70 feet, corresponds to Mpx equal to Fy*Zx, which is equal to 403 Ft.kips, and the Bracing length lr 35.10 ft corresponds to 0.7*Fy*Sx equals 256 Ft.kips. But our W12x65 has an Mn of only 396 ft-kips, an extra length to add to lp.

This distance equals the difference between (403-396)/B.F value. The BF value is the slope of the line joining Lp and Lr and equals 6.02.

The Final L’p=11.86 ft approximated to 11.90 Ft.

Adjustement of Lp value based on Mn .

Check the values for Lp’,lr, and φ*Mn from Table 3-2.

To check Lp’, lr values, and φ*Mn for W12x65, we find the New Lp value equals 11.90 ft, lr=35.10 Ft, and φ*Mn=356 Ft.kips.

Check Lp and lr and φ*Mn.

Check the value for the maximum Total service load.

For Practice problem 5-6-1, what is the available strength for W12x65?We will equate Mult to φ*Mn. We have l/D=3, the uniform ultimate Load Wul=1.2*D+1.6*3D=6D, the Mu=6D*(50)^2/8=356, then D=0.19 K/Ft, the value of L=3*D=3*0.17=0.51 k/F.

The total service load value.

We will add D+L to achieve a Maximum Total service load of 0.76 K/Ft. Thanks a lot.

The PDF used to solve this problem can be viewed or downloaded from the following link.

Here is the link to Chapter 8 – Bending Members section A Beginner’s Guide to the Steel Construction Manual, 14th ed.

Here is the link to Chapter 8 – Bending Members, section, A Beginner’s Guide to the Steel Construction Manual, 15th ed.

Here is the link to Chapter 8 – Bending Members, section, A Beginner’s Guide to the Steel Construction Manual, 16th ed.


For more information about LP and Lr, please see the post: Step-by-step guide to Lateral-torsional buckling.