Pipe and throat areas:
$D = 0.05$ m, $d = 0.02$ m
$A_1 = \frac{\pi D^2}{4} = 1.963 \times 10^{-3}$ m$^2$
$A_2 = \frac{\pi d^2}{4} = 3.142 \times 10^{-4}$ m$^2$
Venturi equation:
\[
Q = C_v A_2 \sqrt{\frac{2\Delta P}{\rho(1-(A_2/A_1)^2)}}
\]
Compute area ratio:
$(A_2/A_1)^2 = (0.3142/1.963)^2 = 0.0256$
Now the flow rate:
\[
Q = 0.98 \times 3.142\times 10^{-4}
\sqrt{\frac{2 \times 50{,}000}{1000(1 - 0.0256)}}
\]
Inside the square root:
\[
\frac{100000}{1000 \times 0.9744} = 102.65
\]
\[
\sqrt{102.65} = 10.13
\]
Thus:
\[
Q = 0.98 \times 3.142\times 10^{-4} \times 10.13
= 3.12 \times 10^{-3} \text{ m}^3\text{/s}
\]
Rounded: $3.12 \times 10^{-3}$ m$^3$ s$^{-1}$