Answer
given,
height = 300 m
speed of aircraft = 40 m/s
propeller rotation = 20 rev/s
moment of inertia = I = 70 Kg/m²
mass = 200 Kg
since no non conservative force act on system, the mechanical energy is conserved after propeller fall off.
by conservation of energy
[tex]E_i = E_f[/tex]
[tex]mgh + \dfrac{1}{2}mv_i^2 + \dfrac{1}{2}I\omega^2_i=\dfrac{1}{2}mv_f^2 + \dfrac{1}{2}I\omega^2_f[/tex]
as there is no air resistance ωi = ωf
[tex]mgh + \dfrac{1}{2}mv_i^2=\dfrac{1}{2}mv_f^2[/tex]
[tex]v_f=\sqrt{v_i^2 + 2gh}[/tex]
[tex]v_f=\sqrt{40^2+ 2\times 9.8 \times 300}[/tex]
[tex]v_f=86.48\ m/s[/tex]
b) the rotation rate of the propeller remains same as there is no air resistance.