Question 6.5: Compute the moment of inertia of the tee shape in Figure 6–1...

Compute the moment of inertia of the tee shape in Figure 6–12 with respect to its centroidal axis.

143801 6-12
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Objective             Compute the moment of inertia.

Given                    Shape shown in Figure 6–12

Analysis                Use the General Procedure listed in this section. As step 1, divide the tee shape into two parts, as shown in Figure 6–13. Part 1 is the vertical stem and part 2 is the horizontal flange.

Results                 The following table summarizes the complete set of data used to compute the total moment of inertia with respect to the centroid of the tee shape. Some of the data are shown also in Figure 6–13. Comments are given here to show the manner of arriving at certain data:

Part A_{i} y_{i} A_{i}  y_{i} I _{i} d_{i} A_{i}  d_{i}^{2} I_{i}+A_{i}  d_{i}^{2}
1 4.0  mm² 2.0  mm 8.0  mm³ 5.333  cm^{4} 0.75 cm 2.25  cm^{4} 7.583  cm^{4}
2 2.0  mm² 4.25  mm 8.50  mm³ 0.042  cm^{4} 1.50 cm 4.50  cm^{4} 4.542  cm^{4}
A_{T} = 6.0  mm² Σ (A_{i}y_{i}) = 16.5  mm³ I_{T} = 12.125 cm^{4}
\bar{Y}  = \frac{∑(A_{i}y_{i})}{A_{T}}= \frac{16.5   mm^{3}}{6.0  mm^{3}} = 2.75 mm

Steps 2 and 3. The first three columns of the table give data for computing the location of the centroid using the technique shown in Section 6–3. Distances, y_{i} , are measured upward from the bottom of the tee. The result is \bar{Y}   = 2.75 cm.

Step 4. Both parts are simple rectangles. Then, the values of I are

I_{1} = bh^{3}/12 = (1.0)(4.0)^{3}/12 = 5.333  cm^{4}

I_{2} = bh^{3}/12 = (4.0)(0.5)^{3}/12 = 0.042  cm^{4}

Step 5. Distances, d_{i} , from the overall centroid to the centroid of each part

d_{1} = \bar{Y} – y_{1} =  2.75 cm – 2.0 cm = 0.75 cm

d_{1} =  y_{2} -\bar{Y}  =  4.25 cm – 2.75 cm = 1.50 cm

Step 6. Transfer term for each part

A_{1}d_{1}^{2} = (4.0  cm^{2})(0.75  cm)^{2} = 2.25  cm^{4}

A_{2}d_{2}^{2} = (4.0  cm^{2})(0.75  cm)^{2} = 2.25  cm^{4}

Step 7. Total moment of inertia

I_{T} = I_{1} + A_{1}d_{1}^{2} + I_{2} + A_{2}d_{2}^{2} 

= 5.333  cm^{4} + 2.25  cm^{4} + 0.042  cm^{4}  + 4.50  cm^{4}

I_{T} = 12.125  cm^{4} 

Comment           Notice that the transfer terms contribute over half of the total value to the moment of inertia.

143801 6-13

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