An airliner arrives at the terminal, and its engines are shut off. The rotor of one of the engines has an initial clockwise angular speed of 2000 rad/s. The engine's rotation slows with an angular acceleration of magnitude 80.0 rad/s2. (a) Determine the angular speed after 10.0 s. (b) How long does it take for the rotor to come to rest?

Respuesta :

(a) 1200 rad/s

The angular acceleration of the rotor is given by:

[tex]\alpha = \frac{\omega_f - \omega_i}{t}[/tex]

where we have

[tex]\alpha = -80.0 rad/s^2[/tex] is the angular acceleration (negative since the rotor is slowing down)

[tex]\omega_f [/tex] is the final angular speed

[tex]\omega_i = 2000 rad/s[/tex] is the initial angular speed

t = 10.0 s is the time interval

Solving for [tex]\omega_f[/tex], we find the final angular speed after 10.0 s:

[tex]\omega_f = \omega_i + \alpha t = 2000 rad/s + (-80.0 rad/s^2)(10.0 s)=1200 rad/s[/tex]

(b) 25 s

We can calculate the time needed for the rotor to come to rest, by using again the same formula:

[tex]\alpha = \frac{\omega_f - \omega_i}{t}[/tex]

If we re-arrange it for t, we get:

[tex]t = \frac{\omega_f - \omega_i}{\alpha}[/tex]

where here we have

[tex]\omega_i = 2000 rad/s[/tex] is the initial angular speed

[tex]\omega_f=0[/tex] is the final angular speed

[tex]\alpha = -80.0 rad/s^2[/tex] is the angular acceleration

Solving the equation,

[tex]t=\frac{0-2000 rad/s}{-80.0 rad/s^2}=25 s[/tex]