[填空题]
A helicopter rotor blade can be considered a lopqfv sl)f6roo(+5-th/m xce -ng thin 2-pa*pzuby y *x6j/wtjmi((h rod, as shown in Fig. 8–4 6 mi/jjt*paz(-xp2byhu (*yw6.
(a) If each of the three rotor helicopter blades is 3.75 m long and has a mass of 160 kg, calculate the moment of inertia of the three rotor blades about the axis of rotation. $kg \cdot m^2$
(b) How much torque must the motor apply to bring the blades up to a speed of 5 $rev/s$ in 8.0 s? $m \cdot N$