Which of the following statements is true?
Shear stress on principal planes is zero.
The question asks to identify the true statement regarding shear stress on principal planes. To answer this, let's first understand what principal planes are in the context of stress analysis.
In a stressed body, at any given point, we can consider different planes passing through that point. On each plane, there will generally be a normal stress (perpendicular to the plane) and a shear stress (parallel to the plane). Principal planes are special planes where the shear stress is zero.
On a principal plane, the stress is purely normal. This purely normal stress is called a principal stress. For a 2D stress state, there are generally two principal planes, which are mutually perpendicular. For a 3D stress state, there are three principal planes, which are mutually orthogonal.
The key characteristic of principal planes is the absence of shear stress.
Let's look at the provided options:
Based on the definition and understanding of principal planes, the shear stress acting on these planes is always zero. This is a fundamental concept in mechanics of materials and theory of elasticity.
Therefore, the statement that is true is that shear stress on principal planes is zero.
| Concept | Description | Shear Stress Value |
|---|---|---|
| Principal Plane | A plane on which the stress is purely normal. | Zero ($\tau = 0$) |
| Principal Stress | The purely normal stress acting on a principal plane. | Not applicable (it's a normal stress) |
| Plane of Maximum Shear Stress | A plane where the shear stress reaches its maximum value. | Maximum ($\tau_{max}$) |
| Normal Stress | Stress component perpendicular to a plane. | Varies |
| Shear Stress | Stress component parallel to a plane. | Varies |
Principal planes and stresses can be found using various methods, such as:
For a 2D stress state ($\sigma_x, \sigma_y, \tau_{xy}$), the shear stress ($\tau_{\theta}$) on a plane at an angle $\theta$ from the x-axis is given by:
$\tau_{\theta} = \frac{\sigma_y - \sigma_x}{2} \sin(2\theta) + \tau_{xy} \cos(2\theta)$
Setting $\tau_{\theta} = 0$ allows us to find the angles ($2\theta$) corresponding to the principal planes.
These methods confirm that principal planes are defined by the condition where shear stress is zero.
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