Chapter 10: Problem 52
Each propeller on a King Air twin-engine airplane consists of three blades, each of mass \(10 \mathrm{kg}\) and length \(125 \mathrm{cm} .\) The blades may be treated approximately as uniform, thin rods, (a) What's the propeller's rotational inertia? (b) If the plane's engine develops a torque of \(2.7 \mathrm{kN} \cdot \mathrm{m}\), how long will it take to spin up the propeller from 1400 rpm to 1900 rpm?