The blades of an aeroplane propeller are 2m long and rotate at 300 rpm.calculate angular velocity and linear velocity of a point on the blades 0.5 m from the tip of the blades
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From the conservation of angular momenta we know,
So at tip of the blade,
I1 *w1 = I2 *w2
where I1 and I2 are the respective angular momentums and w1 and w2 are the angular velicties respectively.
ml^2/3 * 300 = m(0.25l)^2/3 * w
get the value of w from here.\
For Time period it would be: T = 2pi/w
for frequency, f = 1/T
and linear velocity v = w*x where x = 1.5 m from hinge.
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Answer:
Explanation:
The blades make 300 revolutions per minute.
Revolutions per second is :
300 / 60 = 5 revolutions per second.
One revolution = 2π
Hence : 5 × 2π = 10π
Angular velocity = 10 π radians / second
Linear velocity = rw where
w = angular velocity
r = radius from the center
r = 12 - 0.5 = 11.5
V = 11.5 × 10π = 115π
361.28 m/s
Hope it helps!
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