A turbine is developing 7500 kW at 6000 rpm (see Fig, P.14.8). For an allowable shear stress of $1 \times 10^8 \mathrm{~Pa}_3$, what should be the diameter $D_1$ of the shaft transmitting torque from the turbine to the reduction gear system? If the reduction in speed is 100 to 1 , what should be the diameter $D_2$ of the shaft between the reduction gears and the gencrator?
Figure P.148.