Step 1: Understand the velocity distribution in rotational flow.
In a rotational flow (solid body rotation), the tangential velocity \( v \) at a radius \( r \) is given by:
\[
v = \omega r
\]
where \( \omega \) is the angular velocity.
Step 2: Define vorticity.
Vorticity \( \vec{\zeta} \) in 2D flow is:
\[
\zeta = \frac{\partial v}{\partial x} - \frac{\partial u}{\partial y}
\]
But in cylindrical coordinates for rotational flow (where velocity is purely tangential):
\[
\zeta = 2\omega
\]
Step 3: Relate normal velocity gradient to vorticity.
The angular velocity is:
\[
\omega = \frac{1}{2} \zeta
\]
So, the ratio of normal velocity vector (or tangential speed per unit radius \( \frac{v}{r} \)) to angular velocity is:
\[
\frac{v/r}{\omega} = \frac{\omega r / r}{\omega} = \frac{\omega}{\omega} = 1
\]
But the question likely refers to the ratio of the vorticity to angular velocity, which is:
\[
\frac{\zeta}{\omega} = \frac{2\omega}{\omega} = 2
\]
Hence, the required ratio is:
\[
\boxed{2.0}
\]