The shear plane angle \(\phi\) can be calculated using the formula:
\[
\tan \phi = \frac{t_0}{t_c - t_0} \times \frac{\cos \alpha}{\sin \alpha}
\]
Where:
- \(\alpha = 10^\circ\) (rake angle)
- \(t_0 = 0.50 \, \text{mm}\) (chip thickness before the cut)
- \(t_c = 1.125 \, \text{mm}\) (chip thickness after the cut)
Substitute the values into the equation:
\[
\tan \phi = \frac{0.50}{1.125 - 0.50} \times \frac{0.984}{0.173}
\]
Solving this gives:
\[
\phi = 50.4^\circ
\]