5.1 Angular Momentum for a Point Particle
Define the angular momentum L ⃗ S \vec{L}_S L S about the point S S S as the cross product of the vector from S S S to the point particle, r ⃗ S \vec{r}_S r S , and the momentum of the particle, p ⃗ \vec{p} p ,
L ⃗ S = r ⃗ S × p ⃗ . \begin{align*}
\vec{L}_S = \vec{r}_S \times \vec{p}.
\end{align*} L S = r S × p .
Now, let us check out the relation between angular momentum and angular velocity. For simplicity, choose the fixed point to be the origin and the plane spanned by r ⃗ \vec{r} r and v ⃗ \vec{v} v for the polar coordinate system,
L ⃗ = r ⃗ × p ⃗ = m r ⃗ × v ⃗ = m r 2 θ ˙ r ^ × θ ^ = m r 2 θ ˙ k ^ = m r 2 ω ⃗ , \begin{align*}
\vec{L} &= \vec{r} \times \vec{p} \\
&= m \vec{r} \times \vec{v} \\
&= m r^2 \dot{\theta} \hat{r} \times \hat{\theta} \\
&= m r^2 \dot{\theta} \hat{k} \\
&= m r^2 \vec{\omega},
\end{align*} L = r × p = m r × v = m r 2 θ ˙ r ^ × θ ^ = m r 2 θ ˙ k ^ = m r 2 ω ,
where we use the fact that in the polar coordinate system,
v ⃗ = v ⃗ r + v ⃗ θ = r ˙ r ^ + r θ ˙ θ ^ . \begin{align*}
\vec{v} &= \vec{v}_r + \vec{v}_\theta \\
&= \dot{r} \hat{r} + r \dot{\theta} \hat{\theta}.
\end{align*} v = v r + v θ = r ˙ r ^ + r θ ˙ θ ^ .
5.2 Conservation of Angular Momentum
Torque
d L ⃗ S d t = d d t ( r ⃗ S × p ⃗ ) = ( d r ⃗ S d t × p ⃗ ) + ( r ⃗ S × d p ⃗ d t ) . \begin{align*}
\frac{\mathrm{d}\vec{L}_S}{\mathrm{d}t} = \frac{\mathrm{d}}{\mathrm{d}t}(\vec{r}_S \times \vec{p}) = \left( \frac{\mathrm{d}\vec{r}_S}{\mathrm{d}t} \times \vec{p} \right) + \left( \vec{r}_S \times \frac{\mathrm{d}\vec{p}}{\mathrm{d}t} \right).
\end{align*} d t d L S = d t d ( r S × p ) = ( d t d r S × p ) + ( r S × d t d p ) .
d r ⃗ S d t × p ⃗ = v ⃗ × m v ⃗ = 0. \begin{align*}
\frac{\mathrm{d}\vec{r}_S}{\mathrm{d}t} \times \vec{p} = \vec{v} \times m\vec{v} = 0.
\end{align*} d t d r S × p = v × m v = 0.
The rate of angular momentum change about the point S S S is then
d L ⃗ S d t = r ⃗ S × d p ⃗ d t = r ⃗ S × F ⃗ = M ⃗ S . \begin{align*}
\frac{\mathrm{d}\vec{L}_S}{\mathrm{d}t} = \vec{r}_S \times \frac{\mathrm{d}\vec{p}}{\mathrm{d}t} = \vec{r}_S \times \vec{F} = \vec{M}_S.
\end{align*} d t d L S = r S × d t d p = r S × F = M S .
Theorem of Angular Momentum for a Particle
The change in angular momentum is caused by the torque,
J ⃗ S = ∫ t 1 t 2 M ⃗ S d t = L ⃗ S , t 2 − L ⃗ S , t 1 , \begin{align*}
\vec{J}_S = \int_{t_1}^{t_2} \vec{M}_S \mathrm{d}t = \vec{L}_{S,t_2} - \vec{L}_{S,t_1},
\end{align*} J S = ∫ t 1 t 2 M S d t = L S , t 2 − L S , t 1 ,
where J ⃗ S \vec{J}_S J S is defined as the angular impulse about a point S S S .
Theorem (Conservation of Angular Momentum about a Point). If the torque about point S S S is zero,
M ⃗ S = d L ⃗ S d t = 0 , \begin{align*}
\vec{M}_S = \frac{\mathrm{d}\vec{L}_S}{\mathrm{d}t} = 0,
\end{align*} M S = d t d L S = 0 ,
then L ⃗ S = const \vec{L}_S = \text{const} L S = const .
5.3 System of Particles
Theorem of Angular Momentum
The angular momentum L ⃗ S , j \vec{L}_{S,j} L S , j of the j t h j^{th} j t h particle is
L ⃗ S , j = r ⃗ S , j × p ⃗ j . \begin{align*}
\vec{L}_{S,j} = \vec{r}_{S,j} \times \vec{p}_j.
\end{align*} L S , j = r S , j × p j .
L ⃗ S s y s = ∑ j = 1 N L ⃗ S , j = ∑ j = 1 N r ⃗ S , j × p ⃗ j . \begin{align*}
\vec{L}_S^{sys} = \sum_{j=1}^{N} \vec{L}_{S,j} = \sum_{j=1}^{N} \vec{r}_{S,j} \times \vec{p}_j.
\end{align*} L S sys = j = 1 ∑ N L S , j = j = 1 ∑ N r S , j × p j .
d L ⃗ S s y s d t = d d t ∑ j = 1 N L ⃗ S , j = ∑ j = 1 N ( d r ⃗ S , j d t × p ⃗ j + r ⃗ S , j × d p ⃗ j d t ) . \begin{align*}
\frac{\mathrm{d}\vec{L}_S^{sys}}{\mathrm{d}t} = \frac{\mathrm{d}}{\mathrm{d}t} \sum_{j=1}^{N} \vec{L}_{S,j} = \sum_{j=1}^{N} \left( \frac{\mathrm{d}\vec{r}_{S,j}}{\mathrm{d}t} \times \vec{p}_j + \vec{r}_{S,j} \times \frac{\mathrm{d}\vec{p}_j}{\mathrm{d}t} \right).
\end{align*} d t d L S sys = d t d j = 1 ∑ N L S , j = j = 1 ∑ N ( d t d r S , j × p j + r S , j × d t d p j ) .
we have
d L ⃗ S s y s d t = ∑ j = 1 N ( r ⃗ S , j × d p ⃗ j d t ) = ∑ j = 1 N ( r ⃗ S , j × F ⃗ j ) = ∑ j = 1 N ( r ⃗ S , j × ( F ⃗ j e x t + F ⃗ j i n t ) ) = M ⃗ S e x t + M ⃗ S i n t = M ⃗ S e x t . \begin{align*}
\frac{\mathrm{d}\vec{L}_S^{sys}}{\mathrm{d}t} &= \sum_{j=1}^{N} \left( \vec{r}_{S,j} \times \frac{\mathrm{d}\vec{p}_j}{\mathrm{d}t} \right) \\
&= \sum_{j=1}^{N} (\vec{r}_{S,j} \times \vec{F}_j) \\
&= \sum_{j=1}^{N} (\vec{r}_{S,j} \times (\vec{F}_j^{ext} + \vec{F}_j^{int})) \\
&= \vec{M}_S^{ext} + \vec{M}_S^{int} = \vec{M}_S^{ext}.
\end{align*} d t d L S sys = j = 1 ∑ N ( r S , j × d t d p j ) = j = 1 ∑ N ( r S , j × F j ) = j = 1 ∑ N ( r S , j × ( F j e x t + F j in t )) = M S e x t + M S in t = M S e x t .
Theorem. Angular Momentum of a System of Particles about Different Points A and B satisfies
L ⃗ A = L ⃗ B + r ⃗ A , B × p ⃗ s y s . \begin{align*}
\vec{L}_A = \vec{L}_B + \vec{r}_{A,B} \times \vec{p}_{sys}.
\end{align*} L A = L B + r A , B × p sys .
Theorem (Conservation Law of Angular Momentum). For a system of particles, when the net external torque equals zero, the angular momentum of the system becomes constant,
M ⃗ S e x t = 0 ⇒ L ⃗ S s y s = const . \begin{align*}
\vec{M}_S^{ext} = 0 \Rightarrow \vec{L}_S^{sys} = \text{const}.
\end{align*} M S e x t = 0 ⇒ L S sys = const .
Center of Mass Reference Frame
M ⃗ ′ = d L ⃗ ′ d t = ∑ i r ⃗ i ′ × f ⃗ i \begin{align*}
\vec{M}' = \frac{\mathrm{d}\vec{L}'}{\mathrm{d}t} = \sum_{i} \vec{r}'_i \times \vec{f}_i
\end{align*} M ′ = d t d L ′ = i ∑ r i ′ × f i
L ⃗ ′ = ∑ i m i r ⃗ i ′ × v ⃗ i ′ . \begin{align*}
\vec{L}' = \sum_{i} m_i \vec{r}'_i \times \vec{v}'_i.
\end{align*} L ′ = i ∑ m i r i ′ × v i ′ .
M ⃗ i n e r t i a l ′ = ∑ i r ⃗ i ′ × ( − m i a ⃗ c ) = ∑ i − m i r ⃗ i ′ × a ⃗ c = 0 × a ⃗ c = 0. \begin{align*}
\vec{M}'_{inertial} = \sum_{i} \vec{r}'_i \times (-m_i\vec{a}_c) = \sum_{i} -m_i\vec{r}'_i \times \vec{a}_c = 0 \times \vec{a}_c = 0.
\end{align*} M in er t ia l ′ = i ∑ r i ′ × ( − m i a c ) = i ∑ − m i r i ′ × a c = 0 × a c = 0.
Here ( − m i a ⃗ c ) (-m_i\vec{a}_c) ( − m i a c ) is the inertial force. The inertial torque equals 0 since the overall effect of inertial force acts on the center of mass.
The angular momentum of the system in an inertial reference frame is:
L ⃗ = ∑ i m i r ⃗ i × v ⃗ i = ∑ i m i ( r ⃗ i ′ + r ⃗ c ) × ( v ⃗ i ′ + v ⃗ c ) = ∑ i m i r ⃗ i ′ × v ⃗ i ′ + ∑ i m i r ⃗ c × v ⃗ c = L ⃗ ′ + r ⃗ c × p ⃗ c , \begin{align*}
\vec{L} = \sum_{i} m_i \vec{r}_i \times \vec{v}_i = \sum_{i} m_i (\vec{r}'_i + \vec{r}_c) \times (\vec{v}'_i + \vec{v}_c) = \sum_{i} m_i \vec{r}'_i \times \vec{v}'_i + \sum_{i} m_i \vec{r}_c \times \vec{v}_c = \vec{L}' + \vec{r}_c \times \vec{p}_c,
\end{align*} L = i ∑ m i r i × v i = i ∑ m i ( r i ′ + r c ) × ( v i ′ + v c ) = i ∑ m i r i ′ × v i ′ + i ∑ m i r c × v c = L ′ + r c × p c ,
since ∑ i m i r ⃗ i ′ = 0 \sum_i m_i \vec{r}'_i = 0 ∑ i m i r i ′ = 0 and ∑ i m i v ⃗ i ′ = 0 \sum_i m_i \vec{v}'_i = 0 ∑ i m i v i ′ = 0 .