Step 1: Note the plate's stress state.
The plate carries \(\sigma_x = 6.5\) MPa (horizontal faces) and \(\sigma_y = 25\) MPa (vertical faces), with no shear stress on these faces, so these are the principal stresses.
Step 2: Locate the weld's orientation.
The weld runs along the diagonal of the square, which sits at \(45^{\circ}\) to both \(\sigma_x\) and \(\sigma_y\). A plane at \(45^{\circ}\) to the principal directions is exactly the plane of maximum in-plane shear stress.
Step 3: Use the stress transformation equations at \(\theta = 135^{\circ}\), the normal to the weld.
\(\sigma_n = \dfrac{\sigma_x+\sigma_y}{2} + \dfrac{\sigma_x-\sigma_y}{2}\cos2\theta = \dfrac{6.5+25}{2} + \dfrac{6.5-25}{2}\cos270^{\circ} = 15.75 + 0 = 15.75\) MPa, since \(\cos270^{\circ}=0\).
\(\tau = -\dfrac{\sigma_x-\sigma_y}{2}\sin2\theta = -\dfrac{6.5-25}{2}\sin270^{\circ} = -(-9.25)(-1) = -9.25\) MPa.
Step 4: Form the required ratio.
The normal stress perpendicular to the weld is \(15.75\) MPa, and the shear stress along the weld carries a sign of \(-9.25\) MPa under this convention.
Ratio \(= \tau/\sigma_n = -9.25/15.75 = -0.59\).
Final Answer:
Because the weld sits exactly at \(45^{\circ}\) to the principal stresses, it always carries the maximum possible shear stress relative to the local normal stress.
\[ \boxed{\text{ratio} = -0.59} \]