Under Loading–I, the stress state is a uniaxial normal stress along the $x$ direction.
Thus,
\[
\sigma_{xx}^{(I)} = \sigma.
\]
Step 1: Stress transformation for Loading–II.
The second loading applies the same magnitude $\sigma$, but the element is rotated by $45^\circ$.
For a uniaxial stress $\sigma$ rotated by angle $\theta$, the transformed normal stress is:
\[
\sigma_{xx}^{(II)} = \sigma \cos^2\theta.
\]
For $\theta = 45^\circ$,
\[
\cos^2 45^\circ = \frac{1}{2},
\]
so
\[
\sigma_{xx}^{(II)} = \sigma \cdot \frac{1}{2}.
\]
Step 2: Superposition of the two loadings.
Since the structure is linear elastic, stresses add:
\[
\sigma_{xx} = \sigma_{xx}^{(I)} + \sigma_{xx}^{(II)}
= \sigma + \frac{\sigma}{2}
= \frac{3\sigma}{2}.
\]
Step 3: Final conclusion.
The combined normal stress is:
\[
\sigma_{xx} = \frac{3\sigma}{2}.
\]
Final Answer: $3\sigma/2$