In a 2D stress system on an element, if the normal stresses on the x and y axes are \(\sigma_x\) and \(\sigma_y\), and the shear stress is \(\tau\) (\(\tau_{xy}\)), the normal stress on a plane inclined at 45\(^\circ\) to these axes is:
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Stress Transformation. The normal stress on planes of maximum shear stress is equal to the average normal stress: \(\sigma_{avg = (\sigma_x + \sigma_y)/2\). These planes are oriented at 45° to the principal planes. If the given x-y axes are principal axes (\(\tau_{xy=0\)), then the plane at 45° has \(\sigma_n = \sigma_{avg\).
The normal stress (\(\sigma_n\)) on a plane inclined at an angle \(\theta\) with respect to the x-axis is given by the stress transformation equation:
$$ \sigma_{n} = \frac{\sigma_x + \sigma_y}{2} + \frac{\sigma_x - \sigma_y}{2} \cos(2\theta) + \tau_{xy} \sin(2\theta) $$
We are given \(\theta = 45^\circ\). Therefore, \(2\theta = 90^\circ\).
$$ \cos(2\theta) = \cos(90^\circ) = 0 $$
$$ \sin(2\theta) = \sin(90^\circ) = 1 $$
Substituting these values into the equation:
$$ \sigma_{n} = \frac{\sigma_x + \sigma_y}{2} + \frac{\sigma_x - \sigma_y}{2} (0) + \tau_{xy} (1) $$
$$ \sigma_{n} = \frac{\sigma_x + \sigma_y}{2} + \tau_{xy} $$
This result includes the shear stress \(\tau_{xy}\) (represented as \(\tau\) in the options). However, option (2) is \((\sigma_x + \sigma_y)/2\), which is the average normal stress. This value is the normal stress acting on the planes of maximum shear stress *only if* the given x and y axes are the principal axes (meaning \(\tau_{xy} = 0\) initially). Given the options, it is highly probable that the question implies that \(\tau_{xy} = 0\) or is asking for the normal stress on the plane of maximum shear, which is always the average normal stress, \((\sigma_x + \sigma_y)/2\). Assuming this common simplification or interpretation leads to option (2).