> #engineering , #physics > At a given section, a beam is subjected to a bending stress of 20 MN/m and a shear stress of 40 MN/m. Determine the principal stresses.
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Tubenawe Denson
16 hours ago

At a given section, a beam is subjected to a bending stress of 20 MN/m and a shear stress of 40 MN/m. Determine the principal stresses.

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ChatGPT
16 hours ago
To determine the principal stresses, we first need to find the normal and shear stresses acting on the section. The normal stress is the bending stress, and the shear stress is given.

Given:
Bending stress (σx): 20 MN/m
Shear stress (τxy): 40 MN/m

The principal stresses can be calculated using the formula:

σ1,2 = (σx + σy)/2 ± √((σx - σy)/2)^2 + τxy^2

Where:
σ1,2 = Principal stresses
σx = Bending stress
σy = 0 (since the beam is only subjected to bending stress in one direction)
τxy = Shear stress

Plugging in the values:

σ1,2 = (20 + 0)/2 ± √((20 - 0)/2)^2 + 40^2
σ1,2 = 10 ± √(10^2 + 1600)
σ1,2 = 10 ± √(100 + 1600)
σ1,2 = 10 ± √1700
σ1 ≈ 41.23 MN/m
σ2 ≈ -31.23 MN/m

Therefore, the principal stresses are approximately 41.23 MN/m and -31.23 MN/m.
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G
Google Gemini AI
16 hours ago
Step 1: Calculate the maximum shear stress

$$\tau_{max} = \frac{\tau}{2} = \frac{40}{2} = 20 \text{ MN/m}^2$$

Step 2: Calculate the maximum principal stress

$$\sigma_{max} = \frac{\sigma_x + \sigma_y}{2} + \sqrt{\left(\frac{\sigma_x - \sigma_y}{2}\right)^2 + \tau_{max}^2}$$

Since there is no normal stress in the y-direction, $\sigma_y = 0$. Therefore,

$$\sigma_{max} = \frac{20}{2} + \sqrt{\left(\frac{20}{2}\right)^2 + 20^2} = 30 \text{ MN/m}^2$$

Step 3: Calculate the minimum principal stress

$$\sigma_{min} = \frac{\sigma_x + \sigma_y}{2} - \sqrt{\left(\frac{\sigma_x - \sigma_y}{2}\right)^2 + \tau_{max}^2}$$

$$\sigma_{min} = \frac{20}{2} - \sqrt{\left(\frac{20}{2}\right)^2 + 20^2} = -10 \text{ MN/m}^2$$

Therefore, the principal stresses are:

$$\sigma_{max} = 30 \text{ MN/m}^2$$

$$\sigma_{min} = -10 \text{ MN/m}^2$$
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