book:chap5:5.4_center_of_mass_and_spin
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book:chap5:5.4_center_of_mass_and_spin [2022/01/03 14:52] – created jv | book:chap5:5.4_center_of_mass_and_spin [2022/01/06 05:22] (current) – abril | ||
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- | FIXME draft with missing figures and references :!: | ||
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===== 5.4 Center of mass and spin of extended objects | ===== 5.4 Center of mass and spin of extended objects | ||
- | < | + | < |
We consider a setting where there are only long distance force like gravity | We consider a setting where there are only long distance force like gravity | ||
Line 8: | Line 6: | ||
The explicit calculation for the case of gravity in the previous section entails | The explicit calculation for the case of gravity in the previous section entails | ||
that in such a setting the force exerted by a planet on a point particle is identical to the one exerted by a mass point of identical mass | that in such a setting the force exerted by a planet on a point particle is identical to the one exerted by a mass point of identical mass | ||
- | that is located at the center of the planet (see also\cref{quest:volIntegral-professor}e). | + | that is located at the center of the planet (see also [[book:chap5: |
In the present section we therefore explore which effects the force of a point particle exerts on an extended body. | In the present section we therefore explore which effects the force of a point particle exerts on an extended body. | ||
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==== 5.4.1 Evolution of the center of mass ==== | ==== 5.4.1 Evolution of the center of mass ==== | ||
- | The force on the body is described by an integral that takes exactly the same form as\cref{eq:professor-totForce}, | + | The force on the body is described by an integral that takes exactly the same form as [[book:chap5: |
where now $\mathbf q$ is a vector from the point particle to a volume element of the body. | where now $\mathbf q$ is a vector from the point particle to a volume element of the body. | ||
The integral is best evaluated by introducing a coordinate frame $\hat{\boldsymbol e}_1(t), \dots , \hat{\boldsymbol e}_3(t)$ | The integral is best evaluated by introducing a coordinate frame $\hat{\boldsymbol e}_1(t), \dots , \hat{\boldsymbol e}_3(t)$ | ||
with orientation fixed in the rotating body and origin in the body's center of mass | with orientation fixed in the rotating body and origin in the body's center of mass | ||
$\mathbf Q = ( Q_x, Q_y, Q_z )$. | $\mathbf Q = ( Q_x, Q_y, Q_z )$. | ||
- | In immediate generalization of\cref{eq:defCenterMass} | + | In immediate generalization of [[book:chap4: |
\begin{align*} | \begin{align*} | ||
\mathbf Q | \mathbf Q | ||
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with base vectors $\{ \hat{\boldsymbol e}_1, \dots, \hat{\boldsymbol e}_3 \}$ fixed in the body and origin in its center of mass. | with base vectors $\{ \hat{\boldsymbol e}_1, \dots, \hat{\boldsymbol e}_3 \}$ fixed in the body and origin in its center of mass. | ||
Hence, | Hence, | ||
- | \begin{align} \label{eq: | + | <wrap # |
+ | \begin{align} | ||
\mathbf r = \sum_{i=1}^3 r_i \: \hat{\boldsymbol e}_i(t) | \mathbf r = \sum_{i=1}^3 r_i \: \hat{\boldsymbol e}_i(t) | ||
\quad\text{and}\quad | \quad\text{and}\quad | ||
- | \dot{\boldsymbol r} = \sum_{i=1}^3 r_i \: \dot{\hat{\boldsymbol e}}_i(t) | + | \dot{\boldsymbol r} = \sum_{i=1}^3 r_i \: \dot{\hat{\boldsymbol e}}_i(t) |
\\ | \\ | ||
\end{align} | \end{align} | ||
- | | ||
</ | </ | ||
We note that this choice of coordinates entails | We note that this choice of coordinates entails | ||
+ | <wrap # | ||
\begin{align} | \begin{align} | ||
M \, \mathbf Q | M \, \mathbf Q | ||
Line 67: | Line 66: | ||
\Rightarrow\quad | \Rightarrow\quad | ||
0 & | 0 & | ||
- | = \int_{\mathbb R^3} \mathrm{d}^3r \: \rho( \mathbf r ) \: r_i | + | = \int_{\mathbb R^3} \mathrm{d}^3r \: \rho( \mathbf r ) \: r_i \tag{5.4.3} |
- | | + | |
\end{align} | \end{align} | ||
The latter equality holds because a shift of the origin by $\mathbf Q$ | The latter equality holds because a shift of the origin by $\mathbf Q$ | ||
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(i.e., the Jacobi determinant of the transformation is one). | (i.e., the Jacobi determinant of the transformation is one). | ||
The acceleration $\ddot{\boldsymbol q}(t)$ takes the form | The acceleration $\ddot{\boldsymbol q}(t)$ takes the form | ||
+ | |||
+ | <wrap # | ||
+ | |||
\begin{align*} | \begin{align*} | ||
\ddot{\boldsymbol q}(t) = \ddot{\boldsymbol q}(t) + \sum_{i=1}^3 r_i \: \ddot{\hat{\boldsymbol e}}_i(t) | \ddot{\boldsymbol q}(t) = \ddot{\boldsymbol q}(t) + \sum_{i=1}^3 r_i \: \ddot{\hat{\boldsymbol e}}_i(t) | ||
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\nonumber \\ | \nonumber \\ | ||
&= M \: \ddot{\boldsymbol q} + \sum_{i=1}^3 | &= M \: \ddot{\boldsymbol q} + \sum_{i=1}^3 | ||
- | = M \: \ddot{\boldsymbol q} | + | = M \: \ddot{\boldsymbol q} \tag{5.4.4} |
- | | + | |
\end{align} | \end{align} | ||
The overall force $\mathbf F_{\text{tot}}$ results in an acceleration of the center of mass | The overall force $\mathbf F_{\text{tot}}$ results in an acceleration of the center of mass | ||
that behaves exactly as for a point particle described in the previous chapter. | that behaves exactly as for a point particle described in the previous chapter. | ||
- | Thus, we have justified the assumption of point particles adopted in\cref{chapter:EOM}. | + | Thus, we have justified the assumption of point particles adopted in [[book:chap4: |
Line 117: | Line 117: | ||
\end{align*} | \end{align*} | ||
The first summand amounts to the angular momentum of the center of mass, $\mathbf L_{CM} = M \: \mathbf Q | The first summand amounts to the angular momentum of the center of mass, $\mathbf L_{CM} = M \: \mathbf Q | ||
- | The second and the third term vanish due to | + | The second and the third term vanish due to |
The forth term can be simplified by performing the integration in the comoving coordinate frame. | The forth term can be simplified by performing the integration in the comoving coordinate frame. | ||
The coordinate transformation involves a translation by $\mathbf Q$ and rotation. | The coordinate transformation involves a translation by $\mathbf Q$ and rotation. | ||
Hence, the Jacobi determinant is one, and the term only depends on the local coordinates $\mathbf r$. | Hence, the Jacobi determinant is one, and the term only depends on the local coordinates $\mathbf r$. | ||
It is denoted as particle spin. | It is denoted as particle spin. | ||
+ | |||
<WRAP box round> | <WRAP box round> | ||
The //total angular momentum// $\mathbf L_{\text{tot}}$ of a particle can be decomposed into | The //total angular momentum// $\mathbf L_{\text{tot}}$ of a particle can be decomposed into | ||
Line 127: | Line 128: | ||
and its //spin// $\mathbf S$ around the center of mass, $\mathbf Q$, | and its //spin// $\mathbf S$ around the center of mass, $\mathbf Q$, | ||
\begin{align} | \begin{align} | ||
- | \mathbf L_{\text{tot}} &= \mathbf L_{CM} + \mathbf S | + | \mathbf L_{\text{tot}} &= \mathbf L_{CM} + \mathbf S \tag{5.4.5 a} |
\\ | \\ | ||
\text{with}\qquad | \text{with}\qquad | ||
- | \mathbf L_{CM} &= M \: \mathbf Q \times \dot{\boldsymbol q} | + | \mathbf L_{CM} &= M \: \mathbf Q \times \dot{\boldsymbol q} \tag{5.4.5 b} |
\\ | \\ | ||
- | \mathbf S &= \int_{\mathbb R^3} \mathrm{d}^3 r \: \rho( r_1. r_2. r_3 ) \: \mathbf r \times \dot{\boldsymbol r} | + | \mathbf S &= \int_{\mathbb R^3} \mathrm{d}^3 r \: \rho( r_1. r_2. r_3 ) \: \mathbf r \times \dot{\boldsymbol r} \tag{5.4.5 c} |
\end{align} | \end{align} | ||
</ | </ | ||
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As a consequence, | As a consequence, | ||
and the center of mass of the particle can even move in different planes before and after the collision. | and the center of mass of the particle can even move in different planes before and after the collision. | ||
- | This will be demonstrated in the worked example in \cref{section:workedExample-ballReflections}. | + | This will be demonstrated in the worked example in [[book:chap5: |
- | + | ||
</ | </ | ||
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that indicates the rotation axis and angular speed $\left\lvert \mathbf\Omega \right\rvert$, | that indicates the rotation axis and angular speed $\left\lvert \mathbf\Omega \right\rvert$, | ||
and exploring that the relative positions of the mass elements in the body do not change upon rotation. | and exploring that the relative positions of the mass elements in the body do not change upon rotation. | ||
- | Due to \cref{eq: | + | Due to [[#eq_spin-r-rdot |
\begin{align*} | \begin{align*} | ||
\mathbf S | \mathbf S | ||
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The situation simplifies further when one observes | The situation simplifies further when one observes | ||
that the velocities $\dot{\hat{\boldsymbol r}}_k$ are unit vectors | that the velocities $\dot{\hat{\boldsymbol r}}_k$ are unit vectors | ||
- | that must be orthogonal to $\hat{\boldsymbol r}_k$ and to $\Omega$. | + | that must be orthogonal to $\hat{\boldsymbol r}_k$ and to $\Omega$.((Recall that $\hat{\boldsymbol r}_k \cdot \hat{\boldsymbol r}_k = 1$ |
- | \footnote{ | + | |
- | Recall that $\hat{\boldsymbol r}_k \cdot \hat{\boldsymbol r}_k = 1$ | + | |
such that $2 \, \hat{\boldsymbol r}_k \, \cdot \dot{\hat{\boldsymbol r}}_k = 0$, | such that $2 \, \hat{\boldsymbol r}_k \, \cdot \dot{\hat{\boldsymbol r}}_k = 0$, | ||
- | and by construction the motion of mass elements is orthogonal to the axis of rotation. | + | and by construction the motion of mass elements is orthogonal to the axis of rotation.)) |
- | } | + | |
Hence, the velocities can be expressed as | Hence, the velocities can be expressed as | ||
\begin{align*} | \begin{align*} | ||
Line 257: | Line 254: | ||
The finding that the off-diagonal elements of the tensor of inertia vanish is no coincidence. | The finding that the off-diagonal elements of the tensor of inertia vanish is no coincidence. | ||
- | In \cref{exercise:selfTest-inertia-symmetry} | + | In [[book:chap5: |
that this happens whenever the mass distribution features a symmetry in the $ik$ plane. | that this happens whenever the mass distribution features a symmetry in the $ik$ plane. | ||
Moreover, the ...theorem | Moreover, the ...theorem | ||
of linear algebra states | of linear algebra states | ||
that one can always choose coordinates | that one can always choose coordinates | ||
- | where all off-diagonal elements of the tensor of inertia vanish. | + | where all off-diagonal elements of the tensor of inertia vanish((For a general matrix this is not true. |
- | \footnote{For a general matrix this is not true. | + | |
It is a consequence of the fact that $\mathsf\Theta$ is symmetric, i.e., | It is a consequence of the fact that $\mathsf\Theta$ is symmetric, i.e., | ||
- | $\Theta_{ij}=\Theta_{ji}$ for all its entries.} | + | $\Theta_{ij}=\Theta_{ji}$ for all its entries.)). |
The particular axes where this happens are called the axis of inertia of a body. | The particular axes where this happens are called the axis of inertia of a body. | ||
<WRAP box round> | <WRAP box round> | ||
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If the mass distribution of the body obeys reflection or rotation symmetry, | If the mass distribution of the body obeys reflection or rotation symmetry, | ||
the axes of inertia are invariant under the symmetry transformation. | the axes of inertia are invariant under the symmetry transformation. | ||
- | | ||
</ | </ | ||
==== 5.4.3 Time evolution of angular momentum and particle spin ==== | ==== 5.4.3 Time evolution of angular momentum and particle spin ==== | ||
- | <WRAP id=ssection_spinEvolution /> | + | <wrap #ssection_spinEvolution></wrap> |
The angular momentum $\mathbf L_{CM}$ of its center-of-mass motion | The angular momentum $\mathbf L_{CM}$ of its center-of-mass motion | ||
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\dot{\boldsymbol S} | \dot{\boldsymbol S} | ||
= \mathbf M | = \mathbf M | ||
- | = \int_{\text{body}} \mathrm{d}^3 r \; \mathbf r \times \mathbf F( \mathbf Q + \mathbf r ) | + | = \int_{\text{body}} \mathrm{d}^3 r \; \mathbf r \times \mathbf F( \mathbf Q + \mathbf r ) \tag{5.4.6} |
\end{align} | \end{align} | ||
</ | </ | ||
Line 324: | Line 319: | ||
where the gravitational acceleration $\mathbf g$ takes a constant value, | where the gravitational acceleration $\mathbf g$ takes a constant value, | ||
forms a noticeable exception. | forms a noticeable exception. | ||
- | <WRAP box round> | + | |
+ | <WRAP box round> | ||
When an extended body moves subject to a spatially uniform acceleration $\mathbf g$, | When an extended body moves subject to a spatially uniform acceleration $\mathbf g$, | ||
then its center of mass follows a free-flight parabola | then its center of mass follows a free-flight parabola | ||
Line 331: | Line 327: | ||
//Proof.// | //Proof.// | ||
- | The statement about the center-of-mass motion follows from \cref{eq: | + | The statement about the center-of-mass motion follows from [[#eq_body-Ftot |Equation 5.4.4]]. |
Conservation of the spin is due to | Conservation of the spin is due to | ||
\begin{align*} | \begin{align*} |
book/chap5/5.4_center_of_mass_and_spin.1641217963.txt.gz · Last modified: 2022/01/03 14:52 by jv