Step 1: Draw the Mohr's circle for the plate.
With principal stresses $\sigma_x = 6.5$ MPa and $\sigma_y = 25$ MPa and zero shear on the reference faces, the circle has center $C = (\sigma_x+\sigma_y)/2 = 15.75$ MPa and radius $R = (\sigma_y-\sigma_x)/2 = 9.25$ MPa.
Step 2: Place the weld plane on the circle.
A physical rotation of $45^{\circ}$ to reach the weld's normal corresponds to a $90^{\circ}$ rotation on the Mohr's circle, since angles double on the circle. Starting from the $\sigma_x$ point and rotating $90^{\circ}$ lands exactly at the top or bottom of the circle.
Step 3: Read off the stresses at that point.
At the top or bottom of the circle the normal stress equals the center value, $\sigma_n = C = 15.75$ MPa, and the shear stress equals the full radius, $|\tau| = R = 9.25$ MPa, since this is the point of maximum shear on the circle.
Step 4: Take the ratio with the sign from this rotation direction.
Following the convention used, $\tau = -9.25$ MPa while $\sigma_n = 15.75$ MPa stays positive, so the ratio is $-9.25/15.75 = -0.59$.
Final Answer:
Mohr's circle shows directly that a $45^{\circ}$ weld to the principal axes always sits at the point of maximum shear, giving this fixed ratio regardless of how large the actual stresses are.
\[ \boxed{\text{ratio} = -0.59} \]