Question 11.2: A long, slender column ABC is pin-supported at the ends and ...

A long, slender column ABC is pin-supported at the ends and compressed by an axial load P (Fig. 11-15). Lateral support is provided at the midpoint B in the plane of the figure. However, lateral support perpendicular to the plane of the figure is provided only at the ends.

The column is constructed of a steel I-beam section S 200 × 34 having modulus of elasticity E = 200GPa and proportional limit \sigma_{pl} = 300  MPa. The total length of the column is L = 8m.

Determine the allowable load P_{allow} using a factor of safety n = 2.5 with respect to Euler buckling of the column.

11.2
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Use a four-step problem-solving approach.
1. Conceptualize: Because of the manner in which it is supported, this column may buckle in either of the two principal planes of bending. As one possibility, it may buckle in the plane of the figure, in which case the distance between lateral supports is L/2 = 4m and bending occurs about axis 2-2 (see Fig. 11-9c for the mode shape of buckling).

As a second possibility, the column may buckle perpendicular to the plane of the figure with bending about axis 1–1. Because the only lateral support in this direction is at the ends, the distance between lateral supports is L = 8m (see Fig. 11-9b for the mode shape of buckling).

Column properties : From Table F-2(b) obtain the following moments of inertia and cross-sectional area for a S 200 × 34 column:

I_{1}=26.9 \times 10^{6}  mm ^{4} \quad I_{2}=1.78 \times 10^{6}  mm ^{4} \quad A=4360  mm ^{2}

2. Categorize:

Critical loads: If the column buckles in the plane of the figure, the critical load is

P_{ cr }=\frac{\pi^{2} E I_{2}}{(L / 2)^{2}}=\frac{4 \pi^{2} E I_{2}}{L^{2}}

3. Analyze: Substitute numerical values to obtain

P_{ cr }=\frac{4 \pi^{2} E I_{2}}{L^{2}}=\frac{4 \pi^{2}(200  GPa )\left(1.78 \times 10^{6}  mm ^{4}\right)}{(8  m )^{2}}=220  kN

If the column buckles perpendicular to the plane of the figure, the critical load is

P_{ cr }=\frac{\pi^{2} E I_{1}}{L^{2}}=\frac{\pi^{2}(200  GPa )\left(26.9 \times 10^{6}  mm ^{4}\right)}{(8  m )^{2}}=830  kN

Therefore, the critical load for the column (the smaller of the two preceding values) is

P_{ cr }=220  kN

and buckling occurs in the plane of the figure.

Critical stresses: Since the calculations for the critical loads are valid only if the material follows Hooke’s law, verify that the critical stresses do not exceed the proportional limit of the material. For the larger critical load, the critical stress is

\sigma_{ cr }=\frac{P_{ cr }}{A}=\frac{830  kN }{4360  mm ^{2}}=190.4  MPa

Since this stress is less than the proportional limit (\sigma_{pl} = 300  MPa), both critical-load calculations are satisfactory.

4. Finalize:
Allowable load: The allowable axial load for the column, based on Euler buckling, is

P_{\text {allow }}=\frac{P_{ cr }}{n}=\frac{220  kN }{2.5}=88  kN

in which n = 2.5 is the desired factor of safety.

Table F-2(b)
Properties of I-Beam Sections (S Shapes)—SI Units (Abridged List)
Designation Mass
per
Meter
Area Depth Web
Thickness
Flange Axis 1–1 Axis 2–2
Width Thickness I S r I S r
kg mm² mm mm mm mm \times 10^{6} mm^{4} \times 10^{3} mm^{3} mm \times 10^{6} mm^{4} \times 10^{3} mm^{3} mm
S 610 × 149 149 18900 610 18.9 184 22.1 991  3260 229 19.7 215 32.3
S 610 × 119 119 15200 610 12.7 178 22.1 874 2870 241 17.5 197 34.0
S 510 × 143 143 18200 516 20.3 183 23.4 695 2700 196 20.8 228 33.8
S 510 × 112 112 14200 508 16.1 162 20.2 533 2100 194 12.3 152 29.5
S 460 × 104 104 13200 457 18.1 159 17.6 384 1690 170 10.0 126 27.4
S 460 × 81.4 81.4 10300 457 11.7 152 17.6 333 1460 180 8.62 113 29.0
S 380 × 74 74.0 9480 381 14.0 143 15.8 202 1060 146 6.49 90.6 26.2
S 380 × 64 64.0 8130 381 10.4 140 15.8 186 973 151 5.95 85.0 26.9
S 310 × 74 74.0 9420 305 17.4 139 16.7 126 829 116 6.49 93.2 26.2
S 310 × 52 52.0 6580 305 10.9 129 13.8 94.9 624 120 4.10 63.6 24.9
S 250 × 52 52.0 6650 254 15.1 125 12.5 61.2 482 96.0 3.45 55.1 22.8
S 250 × 37.8 37.8 4810 254 7.90 118 12.5 51.2 403 103 2.80 47.4 24.1
S 200 × 34 34.0 4360 203 11.2 106 10.8 26.9 265 78.5 1.78 33.6 20.2
S 200 × 27.4 27.4 3480 203 6.88 102 10.8 23.9 236 82.8 1.54 30.2 21.0
S 150 × 25.7 25.7 3260 152 11.8 90.7 9.12 10.9 143 57.9 0.953 21.0 17.1
S 150 × 18.6 18.6 2360 152 5.89 84.6 9.12 9.16 120 62.2 0.749 17.7 17.8
S 100 × 14.1 14.1 1800 102 8.28 71.1 7.44 2.81 55.4 39.6 0.369 10.4 14.3
S 100 × 11.5 11.5 1460 102 4.90 67.6 7.44 2.52 49.7 41.7 0.311 9.21 14.6
11..2
11...2

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