Concept:
Velocity is a vector quantity. In uniform circular motion, speed remains constant but direction of velocity changes continuously.
Step 1: Initial speed of the aeroplane is:
\[
v=450\ \text{kmph}
\]
Step 2: After half revolution, the aeroplane reaches the diametrically opposite point of the circle.
At this point, velocity direction becomes exactly opposite to the initial velocity.
So:
\[
\vec v_i=450
\]
\[
\vec v_f=-450
\]
Step 3: Change in velocity:
\[
\Delta v=\vec v_f-\vec v_i
\]
\[
\Delta v=-450-450
\]
\[
\Delta v=-900
\]
Magnitude of change in velocity:
\[
|\Delta v|=900\ \text{kmph}
\]
Therefore,
\[
\boxed{900\ \text{kmph}}
\]