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Blades of an airplaneâs engine rotate with an initial speed is 40 rev/min. Assuming constant angular acceleration of magnitude 8 rad/s^2 . (a) how long does it take for the blades to reach the angular speed Ïf = 120 rev/ min?

(b)Through how many radians does a blade turn during the time found in (a).
Note : Write down the detail process

User NicoD
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1 Answer

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Answer:

Part a)

t = 1.05 s

Part b)


\theta = 8.78 rad

Step-by-step explanation:

Initial angular speed is given as


\omega_i = 40 rev/min = 0.66 rev/s


\omega_i = 2\pi (0.66) = 4.19 rad/s

angular acceleration is given as


\alpha = 8 rad/s^2

now we have

part a)

final angular speed = 120 rev/min


\omega_f = 2\pi((120)/(60) rev/s)


\omega_f = 12.57 rad/s

now by kinematics we have


\omega_f = \omega_i + \alpha t


12.57 = 4.19 + 8 t


t = 1.05 s

Part b)

Angle turned by the blades is given by


\theta = \omega_i t + (1)/(2)\alpha t^2


\theta = 4.19(1.05) + (1)/(2)(8)(1.05)^2


\theta = 8.78 rad

User Tessie
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