In: Physics
The propeller of a plane has a rotational inertia of 890 kg*m2. Each blade has a length of 3.3 m. The propellor starts from rest and reaches a final angular speed of 16 rad/s in only 8 seconds.
a) What was the angular acceleration of the propeller?
b) What was the net torque exerted on the propeller while it was accelerating?
c) When t = 4 s, what was ω for the propeller?
d) When t = 4 s, through what angle θ had the propeller rotated? Your answer should be entered in radians.
e) When t = 4 s, determine ac for the tip of a blade.
f) When t = 4 s, determine atan for the tip of a blade.
g) When t = 4 s, determine atot for the tip of a blade.
Thank you for your help!
Rotational inertia of the propeller of the plane = I = 890 kg.m2
Length of each blade = L = 3.3 m
Initial angular speed of the propeller = 1 = 0 rad/s (At rest)
Angular speed of the propeller after 8 sec = 2 = 16 rad/s
Time period = T1 = 8 sec
Angular acceleration of the propeller =
2 = 1 + T1
16 = 0 + (8)
= 2 rad/s2
Net torque on the propeller = net
I = net
(890)(2) = net
net = 1780 N.m
T2 = 4 sec
Angular speed of the propeller at 4 sec = 4
4 = 1 + T2
4 = 0 + (2)(4)
4 = 8 rad/s
Angle through which the propeller has rotated in 4 sec =
= 1T2 + T22/2
= (0)(4) + (2)(4)2/2
= 16 rad
Centripetal acceleration of for the tip of the blade at 4 sec = ac
ac = 42L
ac = (8)2(3.3)
ac = 211.2 m/s2
Tangential acceleration of the tip of blade at 4 sec = atan
atan = L
atan = (2)(3.3)
atan = 6.6 m/s2
Total acceleration of the tip of blade at 4 sec = atot
atot = 211.3 m/s2
a) Angular acceleration of the propeller = 2 rad/s2
b) Net torque exerted on the propeller while accelerating = 1780 N.m
c) Angular speed of the propeller at 4 sec = 8 rad/s
d) Angle through which the propeller has turned in 4 sec = 16 rad
e) Centripetal acceleration of the tip of the blade at 4 sec = 211.2 m/s2
f) Tangential acceleration of the tip of the blade at 4 sec = 6.6 m/s2
g) Total acceleration of the tip of the blade at 4 sec = 211.3 m/s2