For turbines, the speed ratio is related to the square root of the head ratio. We can write the relation as:
\[
\frac{N_1}{N_2} = \sqrt{\frac{H_1}{H_2}}
\]
Where \( N_1 \) is the initial speed (500 rpm), \( N_2 \) is the final speed, \( H_1 \) is the initial head (60 m), and \( H_2 \) is the final head (15 m). Solving, we get:
\[
N_2 = 500 \times \sqrt{\frac{60}{15}} = 250
\]