Question 8.6: Compute the distribution of shearing stress with position in...

Compute the distribution of shearing stress with position in the cross section for a beam with the rectangular shape shown in Figure 8–7. The actual dimensions are 50 mm by 250 mm. Plot the results. The shearing force, V, on the section of interest is 5400 N.

143801 8-7
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Objective              Compute the shearing stress at several axes and plot τ versus position.

Given                    Cross-section shape and dimensions in Figure 8–7. V = 5400 N.

Analysis                Use the Guidelines for Computing Shearing Stresses in Beams. Because the shape is symmetrical with respect to the centroidal axis, we choose to compute the shearing stresses in the upper part at the axes a–a, b–b, c–c, and d–d, as shown in Figure 8–11. Then, the values

of stresses in the lower part at sections b′–b′, c′–c′, and d′–d′ will be the same as the corresponding points computed earlier.

Results                 Step 1. V = 5400 N (given).

Step 2. For the rectangular shape, the centroid is at the midheight, as shown in Figure 8–7, coincident with axis a–a. \bar{Y} =125 mm.

Step 3. I = bh^{3} /12 = (50 mm)(250 mm)³/12 = 6.510 × 10^{7}   mm^{4} .

Step 4. Thickness = t = 50 mm at all axes.

Step 5. We will compute Q = A_{p} y for each axis using the method shown earlier in this chapter. Recall that the value of Q for this section at the centroidal axis was computed in Example Problem 8–1. where we found Q = 390 625 mm³. A similar calculation is summarized in the table following  step 6, using data from Figure 8–11.

Step 6. Using Equation (8–1), the calculation for shearing stress at the neutral axis a–a is  shown here:

\tau = \frac{VQ}{It} = \frac{(5400  N)(390  625  mm^{3})}{(6.51 \times 10^{7}  mm^{4})(50  mm)} = 0.648 N/mm²  = 648 kPa

The calculation would be the same at the other axes with only the value of Q changing. See the following table.

Axis V I t A_{p} y q=A_{p}y \tau = VQ/It (kPa)
a-a 5400 6.51 \times 10^{7} 50 6250 63 390 625 648
b-b 5400 6.51 \times 10^{7} 50 5000 75 375 000 622
c-c 5400 6.51 \times 10^{7} 50 2500 100 250 000 415
d-d 5400 6.51 \times 10^{7} 50 0 125 0 0

The results of shearing stress versus position are shown in Figure 8–12 alongside the rectangular section itself.

Comment             Note that the maximum shearing stress does occur at the neutral axis as predicted. The variation of shearing stress with position is parabolic, ending with zero stress at the top and bottom surfaces.

143801 8-11
143801 8-12

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