The blades of an aeroplane propeller are rotating at the rate of 600 revolutions per minute.
The blades of an aeroplane propeller are rotating at the rate of 600 revolutions per minute. Calculate its angular velocity.
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v = 600 revolutions/min
v = 600/60 revolutions/sec.
w = 2πv = 2 x π x 600/60
w = 20π rad/s
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