An aeroplane is flying with a uniform speed of 100 km/h along the circumference of a circle. The change in velocity in half the revolution will be (in km/h)
300
100
200
150
A
100
B
150
C
300
D
200
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Solution
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Magnitude of velocity(v=100km/h) is same as given flying with a uniform speed.
In the diagram we can see that direction of velocity changes by 180∘,so the ultimate change in velocity is given by Δv
as we can see in the diagram
vB=−vA
⇒Δv=vA−(−vB)⇒Δv=2vA=2×100km/h=200km/h
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