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).