12- Solved problem 5-2 for local buckling of columns.

Last Updated on March 4, 2026 by Maged kamel

A solved problem 5-2 for local buckling of columns.

This is a brief description of the content of post 12- compression.

Brief description for 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.

A Solved problem 5-2 for local buckling of columns.

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.

What is the k value for the column?

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.

Use Table 1-1 part 1- to get the area, flange and web data.

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.

Find bf/2tf, h/tw, rx and ry for the section.

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.

Check column whether elastic or inelastic, and the governing direction.

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.

Graph between KL/r and Fcr/Fy for the given column.

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.

Check the slenderness ratios for flabfe aand web based on B4.1a.

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.

Qs factor relevant equations based on CM#14.

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.

From Table 4-22, get factored stress and Nominal LRFD strength.

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.

From Table 4-22, get factored stress and Nominal ASD Strength.

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.

Using Table 4-1 for the available strength for W12x72


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

The equations for the value of Fcr based on Kl/r value.

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.

Estimation of the Euler stress based on Kl/r value.

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.

Detailed estimate of the nominal strength.

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