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Timothy A. Philpot - Mechanics of materials _ an integrated learning system-John Wiley (2017)

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Lateral

bracing

x

C

B

P

17.5 ft

17.5 ft

z

Strong

axis

y

Weak

axis

W8 × 24

Plan the Solution

If the W8 × 24 column were supported only at its ends, then

buckling about the weak axis of the cross section would be

anticipated. However, additional lateral support is provided to

this column, so the effective length with respect to buckling of

the weak axis is reduced. For this reason, both the effective

length and the radius of gyration with respect to both the strong

and weak axes of the column must be considered. The critical

buckling load will be dictated by the larger of the two effectiveslenderness

ratios.

SolutioN

The following section properties can be obtained from Appendix B

for the W8 × 24 structural steel shape:

z

y

A

x

P

C

I

r

z

z

= 82.7 in. I = 18.3 in.

4 4

y

= 3.42 in. r = 1.61 in.

The subscripts for these properties have been modified to correspond

to the axes shown on the cross section.

Buckling About the Strong Axis

The column could buckle about its strong axis, resulting in the

buckled shape shown in which the column deflects in the x–y

plane. For this manner of failure, the effective length of the

column is KL = 35 ft. The critical buckling load is therefore

y

P

cr

2

2 4

π EIz

π (29,000 ksi)(82.7 in. )

= = = 134.2 kips

2

2

( KL)

[(35 ft)(12 in./ft)]

z

Lateral

bracing

y

B

35 ft

Although we are not required to determine P cr , it is instructive to

calculate the effective-slenderness ratio for buckling about the

strong axis:

(35 ft)(12in./ft)

( KL/ r)

z = = 122.8

3.42 in.

z

A

Buckling about the strong axis.

Buckling About the Weak Axis

Alternatively, the column could buckle about its weak axis. In this case, the column

deflection would occur in the x–z plane as shown in the accompanying figure. For this

manner of failure, the effective length of the column is KL = 17.5 ft. The critical buckling

load about the weak axis is therefore

P

cr

2

π EI 2 4

y π (29,000 ksi)(18.3 in. )

= = = 118.8 kips

2

2

( KL)

[(17.5 ft)(12 in./ft)]

y

The effective-slenderness ratio for buckling about the weak axis is

(17.5 ft)(12 in./ft)

( KL/ r)

y = = 130.4

1.61 in.

The critical load for the column is the smaller of the two load values:

686

P

cr =

118.8 kips

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