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concepts/mechanics/u6/m6-2-angular-momentum.tex
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concepts/mechanics/u6/m6-2-angular-momentum.tex
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\subsection{Angular Momentum and Angular Impulse}
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This subsection connects torque to rotational motion in the same way that linear impulse connects force to linear momentum. The key AP idea is that a net external torque acting for a time interval changes angular momentum about a chosen point.
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\dfn{Angular momentum and angular impulse}{Let $O$ denote a chosen reference point. Let a particle of mass $m$ have position vector $\vec{r}$ measured from $O$, velocity $\vec{v}$, and linear momentum $\vec{p}=m\vec{v}$. The angular momentum of the particle about $O$ is
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\[
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\vec{L}_O=\vec{r}\times \vec{p}.
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\]
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For a system of particles, the total angular momentum about $O$ is
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\[
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\vec{L}_O=\sum_i \vec{r}_i\times \vec{p}_i.
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\]
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Let $\vec{\tau}_{\mathrm{ext},O}(t)$ denote the net external torque about the same point $O$ over a time interval from $t_i$ to $t_f$. The angular impulse about $O$ over that interval is
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\[
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\vec{J}_{\tau,O}=\int_{t_i}^{t_f} \vec{\tau}_{\mathrm{ext},O}\,dt.
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\]
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Its SI unit is $\mathrm{N\cdot m\cdot s}$, which is equivalent to $\mathrm{kg\cdot m^2/s}$. For a rigid body rotating about a fixed axis with moment of inertia $I$ about that axis and angular velocity $\vec{\omega}$, the angular momentum simplifies to
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\[
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\vec{L}=I\vec{\omega}.
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\]
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}
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\thm{Torque-angular momentum relation and angular impulse theorem}{Let $O$ denote a chosen reference point. Let $\vec{L}_O(t)$ be the total angular momentum of a particle or system about $O$, and let $\vec{\tau}_{\mathrm{ext},O}(t)$ be the net external torque about $O$. Then
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\[
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\frac{d\vec{L}_O}{dt}=\vec{\tau}_{\mathrm{ext},O}.
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\]
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Integrating from $t_i$ to $t_f$ gives
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\[
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\Delta \vec{L}_O=\vec{L}_{O,f}-\vec{L}_{O,i}=\int_{t_i}^{t_f} \vec{\tau}_{\mathrm{ext},O}\,dt=\vec{J}_{\tau,O}.
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\]
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For fixed-axis rotation along a chosen axis with unit vector $\hat{k}$, let $\vec{L}=L\hat{k}$ and let $\vec{\tau}_{\mathrm{ext}}=\tau_{\mathrm{ext}}\hat{k}$. Then
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\[
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\frac{dL}{dt}=\tau_{\mathrm{ext}},
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\qquad
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\Delta L=\int_{t_i}^{t_f} \tau_{\mathrm{ext}}\,dt,
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\]
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and if $\tau_{\mathrm{ext}}$ is constant,
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\[
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\Delta L=\tau_{\mathrm{ext}}\Delta t.
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\]
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}
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\nt{Angular momentum and torque depend on the chosen point $O$. The same object can have different $\vec{L}_O$ and $\vec{\tau}_{\mathrm{ext},O}$ when a different origin is chosen, so use the same reference point consistently throughout a problem. The direction of $\vec{L}$ and $\vec{\tau}$ is set by the right-hand rule and is perpendicular to the plane of the relevant cross product. In many AP fixed-axis problems, this vector bookkeeping reduces to signed scalars along one axis: counterclockwise may be chosen positive and clockwise negative. The simplification $\vec{L}=I\vec{\omega}$ is valid for rigid rotation about that fixed axis with the stated moment of inertia about the same axis.}
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\pf{Short derivation from $\vec{L}=\vec{r}\times \vec{p}$}{For one particle about point $O$,
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\[
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\vec{L}_O=\vec{r}\times \vec{p}.
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\]
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Differentiate with respect to time:
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\[
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\frac{d\vec{L}_O}{dt}=\frac{d\vec{r}}{dt}\times \vec{p}+\vec{r}\times \frac{d\vec{p}}{dt}=\vec{v}\times m\vec{v}+\vec{r}\times \vec{F}_{\mathrm{net}}.
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\]
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Because $\vec{v}\times \vec{v}=\vec{0}$,
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\[
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\frac{d\vec{L}_O}{dt}=\vec{r}\times \vec{F}_{\mathrm{net}}=\vec{\tau}_{\mathrm{net},O}.
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\]
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For a system, summing over all particles gives the same form with the net external torque:
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\[
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\frac{d\vec{L}_O}{dt}=\vec{\tau}_{\mathrm{ext},O}.
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\]
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Integrating from $t_i$ to $t_f$ yields
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\[
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\Delta \vec{L}_O=\int_{t_i}^{t_f} \vec{\tau}_{\mathrm{ext},O}\,dt.
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\]
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For a rigid body rotating about a fixed axis with constant moment of inertia $I$,
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\[
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\vec{L}=I\vec{\omega},
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\]
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so along that axis the relation becomes
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\[
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\vec{\tau}_{\mathrm{ext}}=I\vec{\alpha}.
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\]
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}
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\qs{Worked example}{A flywheel rotates about a frictionless fixed axle through its center. Choose counterclockwise as positive, so the axis direction is $\hat{k}$ by the right-hand rule. The flywheel has moment of inertia $I=0.80\,\mathrm{kg\cdot m^2}$ about the axle. Initially its angular velocity is
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\[
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\vec{\omega}_i=12\,\hat{k}\,\mathrm{rad/s}.
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\]
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From $t=0$ to $t=1.5\,\mathrm{s}$, a brake pad exerts a constant external torque
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\[
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\vec{\tau}_{\mathrm{ext}}=-3.2\,\hat{k}\,\mathrm{N\cdot m}.
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\]
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Find:
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\begin{enumerate}[label=(\alph*)]
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\item the angular impulse delivered by the brake,
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\item the flywheel's final angular momentum,
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\item the flywheel's final angular velocity, and
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\item whether the flywheel reverses direction during the interval.
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\end{enumerate}}
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\sol First compute the initial angular momentum using $\vec{L}=I\vec{\omega}$:
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\[
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\vec{L}_i=I\vec{\omega}_i=(0.80\,\mathrm{kg\cdot m^2})(12\,\hat{k}\,\mathrm{rad/s})=9.6\,\hat{k}\,\mathrm{kg\cdot m^2/s}.
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\]
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For part (a), the torque is constant, so the angular impulse is
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\[
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\vec{J}_\tau=\vec{\tau}_{\mathrm{ext}}\Delta t.
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\]
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Thus
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\[
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\vec{J}_\tau=(-3.2\,\hat{k}\,\mathrm{N\cdot m})(1.5\,\mathrm{s})=-4.8\,\hat{k}\,\mathrm{N\cdot m\cdot s}.
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\]
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Using $1\,\mathrm{N\cdot m\cdot s}=1\,\mathrm{kg\cdot m^2/s}$,
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\[
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\vec{J}_\tau=-4.8\,\hat{k}\,\mathrm{kg\cdot m^2/s}.
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\]
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For part (b), apply the angular impulse theorem:
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\[
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\Delta \vec{L}=\vec{J}_\tau=\vec{L}_f-\vec{L}_i.
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\]
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So
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\[
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\vec{L}_f=\vec{L}_i+\vec{J}_\tau=(9.6-4.8)\,\hat{k}\,\mathrm{kg\cdot m^2/s}=4.8\,\hat{k}\,\mathrm{kg\cdot m^2/s}.
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\]
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For part (c), again use $\vec{L}=I\vec{\omega}$:
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\[
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\vec{\omega}_f=\frac{\vec{L}_f}{I}=\frac{4.8\,\hat{k}\,\mathrm{kg\cdot m^2/s}}{0.80\,\mathrm{kg\cdot m^2}}=6.0\,\hat{k}\,\mathrm{rad/s}.
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\]
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For part (d), the final angular velocity still points in the $+\hat{k}$ direction, so the flywheel is still rotating counterclockwise. It slows down, but it does not reverse direction during the $1.5\,\mathrm{s}$ interval.
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The results are
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\[
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\vec{J}_\tau=-4.8\,\hat{k}\,\mathrm{N\cdot m\cdot s},
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\qquad
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\vec{L}_f=4.8\,\hat{k}\,\mathrm{kg\cdot m^2/s},
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\qquad
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\vec{\omega}_f=6.0\,\hat{k}\,\mathrm{rad/s}.
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\]
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This example shows the key AP idea: a torque acting over time changes angular momentum directly, and the sign of the torque determines whether the wheel speeds up or slows down.
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