AP Physics C Mechanics - 5.1 Rotational Kinematics- Exam Style questions- FRQs

Rotational Kinematics AP  Physics C Mechanics FRQ

Unit 5: Torque and Rotational Dynamics

Weightage : 10-15%

AP Physics C Mechanics Exam Style Questions – All Topics

Question

A wind turbine includes a three-blade system that rotates about an axis through the end of each blade, as shown in Figure \(1\). Each blade has a length \(L\) and mass \(M\), with a center of mass located at a distance \(\dfrac{L}{3}\) from the axis of rotation, as shown in Figure \(2\).
(a) Derive an expression for the rotational inertia of the three-blade system. Express your answer in terms of \(M\), \(L\), and physical constants, as appropriate. The rotational inertia of each blade about an axis through its center of mass is given by the equation \(I_{cm}=\dfrac{1}{18}ML^2\).
(b) While the wind blows, the three-blade system operates at a constant angular speed \(\omega_0=2.6\,\text{rad/s}\). The length of one blade is \(L=36\,\text{m}\). The numerical value of the rotational inertia of the system is \(I_{sys}=6.7\times10^6\,\text{kg}\cdot\text{m}^2\). Calculate the time \(T\) it takes the outer edge of a single blade to complete one revolution.
(c) When the wind stops blowing, the angular speed of the system decreases. The angular speed of the system while slowing down is given as a function of time by the equation \(\omega=\omega_0e^{-\beta_0t}\), where \(\beta_0\) is a constant with appropriate units, as shown on the graph in Figure \(3\).
i. Calculate the amount of energy dissipated from \(t=0\), when the wind stops blowing, until the system comes to rest.
ii. Derive an expression for the net torque exerted on the system as a function of \(t\) as the system slows down. Express your answers in terms of \(\beta_0\), \(\omega_0\), \(M\), \(L\), \(I_{sys}\), and physical constants, as appropriate.
iii. Derive an expression for the angular displacement of the system \(\Delta\theta\) as a function of \(t\). Express your answer in terms of \(\beta_0\), \(\omega_0\), \(M\), \(L\), \(I_{sys}\), and physical constants, as appropriate.
(d) The three-blade system is now replaced with a second three-blade system identical to the first, except that the second three-blade system slows down according to the equation \(\omega=\omega_0e^{-\beta t}\), where \(\omega_0=2.6\,\text{rad/s}\) and \(\beta>\beta_0\). The original angular speed function is shown as a dashed line in Figure \(4\). On the graph in Figure \(4\), sketch the angular speed of the second three-blade system as a function of time \(t\).

Most-appropriate topic codes (AP Physics C: Mechanics):

• Topic \(5.4\) — Rotational Inertia (Part \( \mathrm{a} \))
• Topic \(5.1\) — Rotational Kinematics (Parts \( \mathrm{b} \), \( \mathrm{c(iii)} \), \( \mathrm{d} \))
• Topic \(6.1\) — Rotational Kinetic Energy (Part \( \mathrm{c(i)} \))
• Topic \(5.6\) — Newton’s Second Law in Rotational Form (Part \( \mathrm{c(ii)} \))
▶️ Answer/Explanation

(a)
Use the parallel-axis theorem to find the rotational inertia of one blade about the rotation axis:
\( I_{\text{blade}}=I_{CM}+Md^2 \)
\( I_{\text{blade}}=\dfrac{1}{18}ML^2+M\left(\dfrac{L}{3}\right)^2 \)
\( I_{\text{blade}}=\dfrac{1}{18}ML^2+\dfrac{1}{9}ML^2=\dfrac{1}{6}ML^2 \)
Multiply the rotational inertia of one blade by \(3\) to get the total rotational inertia:
\( I_{\text{rotor}}=3I_{\text{blade}}=3\left(\dfrac{1}{6}ML^2\right) \)
\( \boxed{I_{\text{rotor}}=\dfrac{1}{2}ML^2} \)

(b)
The time to complete one revolution is the period \(T\):
\( \omega_0=\dfrac{2\pi}{T} \)
\( T=\dfrac{2\pi}{\omega_0} \)
\( T=\dfrac{2\pi}{2.6\,\text{rad/s}} \)
\( \boxed{T=2.4\,\text{s}} \)

(c)(i)
The amount of energy dissipated is equal to the total initial rotational kinetic energy:
\( E_{\text{dis}}=\Delta K_{\text{rot}} \)
\( E_{\text{dis}}=0-\dfrac{1}{2}I_{sys}\omega_0^2 \)
\( E_{\text{dis}}=-\dfrac{1}{2}(6.7\times 10^6\,\text{kg}\cdot\text{m}^2)(2.6\,\text{rad/s})^2 \)
\( \boxed{E_{\text{dis}}=-2.3\times 10^7\,\text{J}} \)

(c)(ii)
Apply Newton’s second law in rotational form:
\( \tau=I_{sys}\alpha \)
\( \tau=I_{sys}\dfrac{d\omega}{dt} \)
\( \tau=I_{sys}\dfrac{d}{dt}\left(\omega_0e^{-\beta_0t}\right) \)
\( \boxed{\tau=-\beta_0I_{sys}\omega_0e^{-\beta_0t}} \)

(c)(iii)
Integrate the expression for angular speed to find angular displacement:
\( \Delta\theta=\int_0^t \omega(t)\,dt \)
\( \Delta\theta=\int_0^t \omega_0e^{-\beta_0t}\,dt \)
\( \Delta\theta=\left[-\dfrac{\omega_0}{\beta_0}e^{-\beta_0t}\right]_0^t \)
\( \Delta\theta=-\dfrac{\omega_0}{\beta_0}e^{-\beta_0t}-\left(-\dfrac{\omega_0}{\beta_0}(1)\right) \)
\( \boxed{\Delta\theta=\dfrac{\omega_0}{\beta_0}\left(1-e^{-\beta_0t}\right)} \)

(d)
Draw a continuous curve showing an exponential decay. Because \(\beta>\beta_0\), the new system slows down faster. The new curve must start at the same initial angular speed, \(\omega_0=2.6\,\text{rad/s}\), and decay entirely below the original dashed curve.

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