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?

Short Answer

Expert verified
The rotational inertia of the propeller is calculated first. Using the given torque, the angular acceleration is computed. Finally, after converting the initial and final speeds from rpm to rad/s, the time it takes for the propeller to reach the desired speed is calculated.

Step by step solution

01

Calculate the Moment of Inertia of the Propeller

The moment of inertia, \(I\), of a rod of mass, \(m\), and length, \(l\), about an axis through one end perpendicular to the length is given as \(I = \frac{1}{3}ml^2\). Given mass of the blade (\(m\)) is 10 kg and length of the blade (\(l\)) is 125 cm = 1.25 m, the moment of inertia for one blade would be calculated as \(I = \frac{1}{3}(10)(1.25)^2\). The propeller includes three blades, so the total moment of inertia will be 3 times this amount.
02

Calculate the Angular Acceleration

Torque (\(\tau\)) is equal to the Moment of inertia (\(I\)) times angular acceleration (\(\alpha\)), represented as \(\tau = I\alpha\). Given Torque (\(\tau\)) is 2.7 kN.m = 2700 N.m, we can calculate the angular acceleration from this formula as \(\alpha = \frac{\tau}{I}\).
03

Calculate the Time to Spin up the Propeller

Angular speed is measured in rad/s, so we first convert the given rpm to rad/s. The initial angular speed (\(\omega_{i}\)) is 1400 rev/min and the final angular speed (\(\omega_{f}\)) is 1900 rev/min. To convert them to rad/s, use the relation 1 rev = \(2\pi\) rad and 1 min = 60 s. Then use the angular form of the second equation of motion (\(\omega_{f} = \omega_{i} + \alpha t\)) to find the time (\(t\)).

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