To find the circulation \( \Gamma \) around the spinning circular cylinder, we use the relationship between the lift per unit span and circulation for a cylinder in potential flow:
\[
{Lift per unit span} = \rho \cdot \Gamma \cdot V_\infty
\]
Where:
\( {Lift per unit span} = 6 \, {N/m} \),
\( \rho = 1.225 \, {kg/m}^3 \) (density of air),
\( V_\infty = 30 \, {m/s} \) (free-stream velocity),
\( \Gamma \) is the circulation.
Rearranging the formula to solve for \( \Gamma \):
\[
\Gamma = \frac{{Lift per unit span}}{\rho \cdot V_\infty}
\]
Substituting the given values:
\[
\Gamma = \frac{6}{1.225 \times 30} = \frac{6}{36.75} \approx 0.163 \, {m}^2/{s}
\]
When rounded to two decimal places, the circulation is approximately 0.16 m\(^2\)/s.