Question:

An aeroplane is moving in a circular path with a speed of \(450\ \text{kmph}\). What is the change in velocity in half revolution?

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In half revolution of circular motion, velocity reverses direction, so change in velocity is \(2v\).
  • \(0\ \text{kmph}\)
  • \(450\ \text{kmph}\)
  • \(250\ \text{kmph}\)
  • \(900\ \text{kmph}\)
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The Correct Option is D

Solution and Explanation

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, \[ \boxed{900\ \text{kmph}} \]
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