Last Updated on March 4, 2026 by Maged kamel
- A solved problem 5-2 for local buckling of columns.
- Detailed data for the solved problem 5-2 for local buckling of columns.
- 1-What is the K value for the column?
- 2-Check the bf/2tf, h/tw, rx, and ry for the column.
- 3-Check whether the column is slender or not.
- 4-Using Table 4-22 for the available critical stress for compression members.
- If using Table 4-1 for the solved problem 5-2 for local buckling.
- If Using the general provision for the available strength.
- Detailed data for the solved problem 5-2 for local buckling of columns.
A solved problem 5-2 for local buckling of columns.
This is a brief description of the content of post 12- compression.

Detailed data for the solved problem 5-2 for local buckling of columns.
A solved problem for local buckling 5-2, from Prof. Jack McCormac’s handbook.
For the column shown in Figure 5.8, if 50 ksi steel is used.
a) Using the column critical stress values in Table 4-22 of the Manual, determine the LRFD design strength Φ Pn and the ASD allowable strength P/Ωc, for the column shown in Figure 5.8.
b) Repeat the problem by using Table 4-1 of the Manual.
c) Solve by using the AISC equation E3.

1-What is the K value for the column?
Referring to the given section of W12x72, Height is 15 feet, fixed from the bottom and hinged from the top, kx=ky=0.7. But, the recommended values for kx and Ky are taken to be equal to 0.80.

Using Table 1-1 part 1-for the properties of the section, the flange width, bf=12 inch, the thickness of the flange is 0.67, the web thickness is equal to 0.43, and the overall height d=12.3 inch. There is no C note in the section, which means that the section is non-slender, but we will double-check the slenderness later.

2-Check the bf/2tf, h/tw, rx, and ry for the column.
Using Table 1-1 part 2-for the properties of the section, bf/2tf=8.99, hw/tw=22.60, the radius of gyration about the x-direction, rx=5.31 inches, and the radius of gyration about the Y-direction, ry=3.04 inches.

We have to determine whether the column is elastic or inelastic. We estimate the controlling lambda=4.71*sqrt(E/Fy)=4.71*sqrt(29000/50)=113.19. Estimate Kl/rx and Kl/ry and check which value is bigger, Kl/rx=27.12. At the same time, Kl/ry = 47.36; the design is controlled by buckling in the Y direction, and the column is a short column.

Please refer to the slide image that shows the relation between Kl/r and the ratio of fcr/Fy. Fcr/Fy will be >0.39 but less than 1.

3-Check whether the column is slender or not.
Check the ratio b/t should be <=0.56*sqrt(E/Fy),The limiting Kl/r = 0.56 *sqrt (E/fy)=0.56 *sqrt (29000/50) = 13.48. The b/t equals 8.99. The Flange is not slender. There is another check for h/tw that should be <= 1.496*sqrt(E/Fy), which is 35.88.
The h/tw from the table is 22.60, which is less than 35.88; then the whole section is non-slender.

The Qs is equal to 1.0, based on CM#14 when b/t is less than 0.56*sqrt(E/Fy). Please refer to the following slide image for more details.

4-Using Table 4-22 for the available critical stress for compression members.
Refer to the table for the kl/r, and for Fy=50 ksi, our kl/r about the Y-axis is 47.37. This value is within the range of 47 and 48.
The Table will give Fcr corresponding to both the LRFD and ASD. For LRFD, the factored stress is between 38.3 ksi and 38.0 ksi by interpolation.
We will get the value of 38.189 ksi for the LRFD of the solved problem 5-2 for local buckling.
To estimate Φc* Pn=Φc*Fcr*Ag=38.189*21.10=806 kips.

For ASD, refer to the table for the kl/r, and for Fy=50 ksi, our kl/r about the Y-axis is 47.37. This value is within the range of 47 and 48.
The Table will give Fcr corresponding to both the LRFD and ASD. For LRFD, the factored stress is between 25.50 ksi and 25.30 ksi by interpolation.
We will get the value of Pn/Ω=536.0 kips.

If using Table 4-1 for the solved problem 5-2 for local buckling.
Then, for part b, for the solved problem 5-2, using Table 4-1, as part b for the solved problem, the main difference between the two tables is that Table 4-1 uses the coefficient Kl, not Kl/r as used by Table 4-22, previously our K*l/r=47.37, while our kl= 0.8* 15=12 feet. From Kl=12 ft, draw a line that will intersect with a vertical line passing by W12x72.
The intersection of the two lines yields a value of 806 kips for the LRFD design. and 536 kips for the ASD design, the same values obtained from Table 4-22 item a, these values match each other.

If Using the general provision for the available strength.
In the third step, it is required to estimate the values using the general equation, which is part c for the solved problem 5-2. Please find the related equations for the estimation of Fcr values

For the general equation, for the short column, we are dealing with the curve at the left side of the 113.43 line.The column is short, Fe=Pi^2E/(kl/r)^2=(Pi)^2(29000)/(47.37)^2, the FE value equals 127.553 ksi.

Fcr=0.658^(50/127.6557), all multiplied by(50), fcr=42.434 ksi, to be multiplied by phi=0.9 by area=21.1 inch2. We get Φ*Pn =806 kips for the LRFD.
In the case of ASD, for Ω=1.67, then Pn/Ω=42.434*(21.1)/1.67= Pn/Ω=536.14 kips, which matches the values obtained from Table 4-22 and Table 4-1.

The Pdf of this post can be viewed and downloaded from the next document.
The next post: solved problem 5-3 for local buckling.
For a good A Beginner’s Guide to the Steel Construction Manual, 14th ed. Chapter 7 – Concentrically Loaded Compression Members.
For a good A Beginner’s Guide to the Steel Construction Manual, 15th ed. Chapter 7 – Concentrically Loaded Compression Members.
For a good A Beginner’s Guide to the Steel Construction Manual, 16th ed. Chapter 7 – Concentrically Loaded Compression Members.