Difference between revisions of "D8. Conservation of dynamic magnitudes"

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====✏️ Exemple D8.5: col·lisió d’una anella i un braç ====
====✏️ EXAMPLE D8.5: collision of a ring and an articulated arm====
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:A negative value for n means that the '''ICR''' is located at a distance e above <math>\Ps</math>.
:A negative value for n means that the '''ICR''' is located at a distance e above <math>\Ps</math>.


:[[File:ExD8-5-3-eng-esp.png|thumb|center|500px|link=]]
:[[File:ExD8-5-3-eng.png|thumb|center|500px|link=]]


:Before the collision <math>\ts_\mathrm{before}</math>, <math>\Os</math> is not a point fixed to the ring in general (it is not its '''ICR'''). Its angular momentum has to be calculated thorugh <span style="text-decoration: underline;"> [[D4. Teoremes vectorials#D4.8 Descomposició baricèntrica del moment cinètic|'''barycentric decomposition ''']]</span>.  The initial angular momentum of the arm is zero because it does not move:
:Before the collision <math>\ts_\mathrm{before}</math>, <math>\Os</math> is not a point fixed to the ring in general (it is not its '''ICR'''). Its angular momentum has to be calculated thorugh <span style="text-decoration: underline;"> [[D4. Teoremes vectorials#D4.8 Descomposició baricèntrica del moment cinètic|'''barycentric decomposition ''']]</span>.  The initial angular momentum of the arm is zero because it does not move:

Revision as of 17:36, 4 November 2024

[math]\displaystyle{ \newcommand{\uvec}{\overline{\textbf{u}}} \newcommand{\vvec}{\overline{\textbf{v}}} \newcommand{\evec}{\overline{\textbf{e}}} \newcommand{\Omegavec}{\overline{\mathbf{\Omega}}} \newcommand{\velang}[2]{\Omegavec^{\textrm{#1}}_{\textrm{#2}}} \newcommand{\Alfavec}{\overline{\mathbf{\alpha}}} \newcommand{\accang}[2]{\Alfavec^{\textrm{#1}}_{\textrm{#2}}} \newcommand{\ds}{\textrm{d}} \newcommand{\ps}{\textrm{p}} \newcommand{\ns}{\textrm{n}} \newcommand{\hs}{\textrm{h}} \newcommand{\cs}{\textrm{c}} \newcommand{\gs}{\textrm{g}} \newcommand{\Ns}{\textrm{N}} \newcommand{\Hs}{\textrm{H}} \newcommand{\Fs}{\textrm{F}} \newcommand{\ms}{\textrm{m}} \newcommand{\ts}{\textrm{t}} \newcommand{\us}{\textrm{u}} \newcommand{\vs}{\textrm{v}} \newcommand{\Rs}{\textrm{R}} \newcommand{\Ts}{\textrm{T}} \newcommand{\Ls}{\textrm{L}} \newcommand{\As}{\textrm{A}} \newcommand{\Ds}{\textrm{D}} \newcommand{\Bs}{\textrm{B}} \newcommand{\es}{\textrm{e}} \newcommand{\fs}{\textrm{f}} \newcommand{\is}{\textrm{i}} \newcommand{\Is}{\textrm{I}} \newcommand{\ks}{\textrm{k}} \newcommand{\js}{\textrm{j}} \newcommand{\rs}{\textrm{r}} \newcommand{\ss}{\textrm{s}} \newcommand{\Os}{\textbf{O}} \newcommand{\Gs}{\textbf{G}} \newcommand{\Cbf}{\textbf{C}} \newcommand{\Or}{\Os_\Rs} \newcommand{\Qs}{\textbf{Q}} \newcommand{\Cs}{\textbf{C}} \newcommand{\Ps}{\textbf{P}} \newcommand{\Ss}{\textbf{S}} \newcommand{\Js}{\textbf{J}} \newcommand{\P}{\textrm{P}} \newcommand{\Q}{\textrm{Q}} \newcommand{\Ms}{\textrm{M}} \newcommand{\deg}{^\textsf{o}} \newcommand{\xs}{\textsf{x}} \newcommand{\ys}{\textsf{y}} \newcommand{\zs}{\textsf{z}} \newcommand{\dert}[2]{\left.\frac{\ds{#1}}{\ds\ts}\right]_{\textrm{#2}}} \newcommand{\ddert}[2]{\left.\frac{\ds^2{#1}}{\ds\ts^2}\right]_{\textrm{#2}}} \newcommand{\vec}[1]{\overline{#1}} \newcommand{\vecbf}[1]{\overline{\textbf{#1}}} \newcommand{\vecdot}[1]{\overline{\dot{#1}}} \newcommand{\OQvec}{\vec{\Os\Qs}} \newcommand{\GQvec}{\vec{\Gs\Qs}} \newcommand{\GPvec}{\vec{\Gs\Ps}} \newcommand{\PSvec}{\vec{\Ps\Ss}} \newcommand{\QQvec}{\vec{\Qs\Qs}} \newcommand{\QGvec}{\vec{\Qs\Gs}} \newcommand{\QPvec}{\vec{\Qs\Ps}} \newcommand{\JQvec}{\vec{\Js\Qs}} \newcommand{\GJvec}{\vec{\Gs\Js}} \newcommand{\OPvec}{\vec{\Os\textbf{P}}} \newcommand{\OCvec}{\vec{\Os\Cs}} \newcommand{\OGvec}{\vec{\Os\Gs}} \newcommand{\GCvec}{\vec{\Gs\Cs}} \newcommand{\PGvec}{\vec{\Ps\Gs}} \newcommand{\abs}[1]{\left|{#1}\right|} \newcommand{\braq}[2]{\left\{{#1}\right\}_{\textrm{#2}}} \newcommand{\matriz}[9]{ \begin{bmatrix} {#1} & {#2} & {#3}\\ {#4} & {#5} & {#6}\\ {#7} & {#8} & {#9} \end{bmatrix}} \newcommand{\diag}[3]{ \begin{bmatrix} {#1} & {0} & {0}\\ {0} & {#2} & {0}\\ {0} & {0} & {#3} \end{bmatrix}} \newcommand{\vector}[3]{ \begin{Bmatrix} {#1}\\ {#2}\\ {#3} \end{Bmatrix}} \newcommand{\vecdosd}[2]{ \begin{Bmatrix} {#1}\\ {#2} \end{Bmatrix}} \newcommand{\vel}[2]{\vvec_{\textrm{#2}} (\textbf{#1})} \newcommand{\acc}[2]{\vecbf{a}_{\textrm{#2}} (\textbf{#1})} \newcommand{\accs}[2]{\vecbf{a}_{\textrm{#2}}^{\textrm{s}} (\textbf{#1})} \newcommand{\accn}[2]{\vecbf{a}_{\textrm{#2}}^{\textrm{n}} (\textbf{#1})} \newcommand{\velo}[1]{\vvec_{\textrm{#1}}} \newcommand{\accso}[1]{\vecbf{a}_{\textrm{#1}}^{\textrm{s}}} \newcommand{\accno}[1]{\vecbf{a}_{\textrm{#1}}^{\textrm{n}}} \newcommand{\re}[2]{\Re_{\textrm{#2}}(\textbf{#1})} \newcommand{\psio}{\dot{\psi}_0} \newcommand{\Pll}{\textbf{P}_\textrm{lliure}} \newcommand{\agal}[1]{\vecbf{a}_{\textrm{Gal}} (#1)} \newcommand{\angal}[1]{\vecbf{a}_{\textrm{NGal}} (#1)} \newcommand{\vgal}[1]{\vecbf{v}_{\textrm{Gal}} (#1)} \newcommand{\fvec}[2]{\overline{\mathbf{F}}_{\textrm{#1}\rightarrow\textrm{#2}}} \newcommand{\mvec}[2]{\overline{\mathbf{M}}_{\textrm{#1}\rightarrow\textrm{#2}}} }[/math]


The vector theorems relate the variation of two dynamic magnitudes ([math]\displaystyle{ \overline{\Ds\Ms} }[/math]) that depend on the mass geometry and the motion of the system (the linear momentum and the angular momentum) with the resultant of the external actions on the system [math]\displaystyle{ (\sum \overline{\As\mathrm{C}_\mathrm{ext}}) }[/math] ( [math]\displaystyle{ \sum \overline{\As\mathrm{C}_\mathrm{ext}} }[/math] includes the external interactions and, if working in a non-Galilean reference frame,the associated inertial actions). In a generic way, these theorems can be written in the following form:

[math]\displaystyle{ \sum \overline{\As\mathrm{C}_\mathrm{ext}}=\dert{\overline{\Ds\Ms}}{R}. }[/math]


When in a direction fixed to the reference frame R(dfR) direction fixed to the reference frame R is conserved:[math]\displaystyle{ \left. \sum \overline{\As\mathrm{C}_\mathrm{ext}}\right]_\mathrm{dfR}=0 \Rightarrow \left. \overline{\Ds\Ms}\right]_\mathrm{dfR}=\text{constant} }[/math].

A conservation is an interesting property: it allows one to ignore the evolution of the system for a finite time and maintain a partial knowledge (if not all the components of [math]\displaystyle{ \overline{\Ds\Ms} }[/math]) are conserved) or a total knowledge (if the conservation occurs in the three directions of the space of R) of the system’s state.

Two important things have to be kept in mind when it comes to invoking conservations:

  • We have to be sure that the component of the external actions that is zero corresponds to a direction fixed in the reference frame (a zero value in a direction variable with respect to R means that the [math]\displaystyle{ \overline{\Ds\Ms} }[/math] component in that direction has a constant value, but not a constant direction!).
  • We have to remember that conservation refers to a dynamic magnitude and not a kinematic one (in principle). When the [math]\displaystyle{ \overline{\Ds\Ms} }[/math] is the linear momentum [math]\displaystyle{ (\overline{\Ds\Ms}=\Ms\vel{G}{R}) }[/math], as it is proportional to the velocity of the center of mass, the corresponding component of [math]\displaystyle{ \vel{G}{R} }[/math] is conserved. When it is the angular momentum of a single rigid body about a point that belongs to that rigid body [math]\displaystyle{ \overline{\Ds\Ms} }[/math] since in general it is not proportional to the angular velocity [math]\displaystyle{ (\overline{\Ds\Ms}=\overline{\mathrm{H}}_\mathrm{RTQ}(\Qs),\Qs \in \mathrm{S}) }[/math] the conservation of [math]\displaystyle{ \overline{\Ds\Ms} }[/math] does not imply that of [math]\displaystyle{ \velang{S}{R} }[/math].

Conservations are often the consequence of simplifications in the formulation of problems, such as neglecting friction. In real life, in general nothing is conserved.

💭 Proof ➕

Let’s project the vector thorem in a vector basis with a dierction fixed to the reference frame (for example, direction3):

[math]\displaystyle{ \sum \overline{\As\mathrm{C}_\mathrm{ext}}=\dert{\overline{\Ds\Ms}}{R} \quad \Rightarrow \quad \vector{\sum\As\mathrm{C}_1}{\sum\As\mathrm{C}_2}{\sum\As\mathrm{C}_3}=\left\{\dert{\overline{\Ds\Ms}}{R}\right\}=\vector{\dot{\Ds\Ms_1}}{\dot{\Ds\Ms_2}}{\dot{\Ds\Ms_3}}+\left\{\velang{B}{R}\right\}\times \vector{\Ds\Ms_1}{\Ds\Ms_2}{\Ds\Ms_3} }[/math]

Since direction 3 is fixed to R, the angular velocity of the vector basis relative to R [math]\displaystyle{ \velang{B}{R} }[/math] must have a component in that direction. Therefore:

[math]\displaystyle{ \vector{\sum\As\mathrm{C}_1}{\sum\As\mathrm{C}_2}{\sum\As\mathrm{C}_3}=\left\{\dert{\overline{\Ds\Ms}}{R}\right\}=\vector{\dot{\Ds\Ms_1}}{\dot{\Ds\Ms_2}}{\dot{\Ds\Ms_3}}=\vector{0}{0}{\Omega_3}\times \vector{\Ds\Ms_1}{\Ds\Ms_2}{\Ds\Ms_3}= \vector{\dot{\Ds\Ms_1}-\Omega_3\cdot\Ds\Ms_2}{\dot{\Ds\Ms_2}-\Omega_3\cdot\Ds\Ms_1}{\dot{\Ds\Ms_3}} }[/math]


Si [math]\displaystyle{ \sum \As\mathrm{C}_3=0 \quad \Rightarrow \quad \dot{\Ds\Ms_3}=0 \quad \Rightarrow \quad \Ds\Ms_3=\text{CONSTANT!}. }[/math]


However, if [math]\displaystyle{ \sum \As\mathrm{C}_1 }[/math] or [math]\displaystyle{ \sum \As\mathrm{C}_2 }[/math] are zero, the corresponding components in [math]\displaystyle{ \overline{\Ds\Ms} }[/math] ( [math]\displaystyle{ \Ds\Ms_1 }[/math] or [math]\displaystyle{ \Ds\Ms_2 }[/math]) are not constant in principle:


[math]\displaystyle{ \sum \As\mathrm{C}_1=0 \quad \Rightarrow \quad \dot{\Ds\Ms_1}-\Omega_3\cdot\Ds\Ms_2 =0 \quad \Rightarrow \quad \dot{\Ds\Ms_1}=\Omega_3\cdot\Ds\Ms_2 \quad \Rightarrow \quad \Ds\Ms_1 \neq \text{constant}, }[/math]

[math]\displaystyle{ \sum \As\mathrm{C}_2=0 \quad \Rightarrow \quad \dot{\Ds\Ms_2}+\Omega_3\cdot\Ds\Ms_1 =0 \quad \Rightarrow \quad \dot{\Ds\Ms_2}=-\Omega_3\cdot\Ds\Ms_1 \quad \Rightarrow \quad \Ds\Ms_2 \neq \text{constant} . }[/math]



D8.1 Examples

✏️ EXAMPLE D8.1: person jumping on a platform


ExD8-1-1-eng.png
A person of mass M, moving at speed [math]\displaystyle{ \mathrm{v}_0 }[/math] on a smooth ground [math]\displaystyle{ (\mu=0) }[/math], jumps onto a platform of mass m which is initially at rest with respect to the floor, and comes to rest relative to it. We want to investigate the evolution of the motion of these two elements (person and platform).
Is the linear momentum conserved?.
The person's jump takes place on a smooth ground that does not introduce any horizontal force on the person or on the platform. Therefore, during the jump and for the SYSTEM (person + platform) and the ground reference frame:
[math]\displaystyle{ \left.\sum \overline{\Fs}_\mathrm{ext}\right]_\mathrm{horizontal}=0 \quad \Rightarrow \quad }[/math] CONSTANT horizontal linear momentum relative to the ground!
Before jumping [math]\displaystyle{ (\ts_\mathrm{inicial}) }[/math], the linear momentum (relative to the ground) is only associated with the person: [math]\displaystyle{ (\rightarrow \ms\vs_0) }[/math]. Just after jumping [math]\displaystyle{ (\ts_\mathrm{final}) }[/math], as the person is at rest relative to the platform, both elements move with the same velocity relative to the ground [math]\displaystyle{ \left[\rightarrow (\Ms+\ms)\vs \right]. }[/math].
ExD8-1-2-eng.png
The conservation of the horizontal linear momentum between these two time instants allows us to calculate the final velocity of the system: [math]\displaystyle{ (\rightarrow \ms\vs_0) = \left[\rightarrow (\Ms+\ms)\vs \right] \quad \Rightarrow \quad \vs=\frac{\ms}{\Ms+\ms}\vs_0. }[/math].
This speed is constant while the system slides on the smooth ground, but as soon as it enters the rough area [math]\displaystyle{ (\mu \neq 0) }[/math], that will change: the friction force of the ground on the platform, horizontal and opposite to [math]\displaystyle{ \overline{\vs}_\Ts }[/math] (platform) will make it decrease. The linear momentum is no longer conserved:
[math]\displaystyle{ \overline{\Fs}_\mathrm{ground \rightarrow syst}=(\leftarrow \Fs_\mathrm{friction})=(\Ms+\ms)\acc{G}{E}. }[/math]
The horizontal linear momentum of the person and the platform (separately) are not conserved during the jump because of the horizontal constraint forces that appear between them when the person-platform contact begins.
ANIMACIONS

✏️ EXAMPLE D8.2: stopping a block on a wagon


ExD8-2-1-eng.png
A person stands on a wagon, both initially at rest relative to the ground. The mass of the system (person + wagon) is M, and the wheels of the wagon are massless. The block, with mass m, has an initial velocity [math]\displaystyle{ \vs_0 }[/math] relative to the ground directed towards the person, which stops it relative to the platform. The friction associated with the joints between wheels and wagon is neglected. We want to investigate the evolution of the movement of the system.
Is the linear momentum conserved?.
The wheels are Auxiliary Constraint Elements (ACE) and cannot transmit horizontal forces (see example D3.10). Hence, for the SYSTEM (person + wagon with wheels + block) and the ground reference frame:
[math]\displaystyle{ \left.\sum \overline{\Fs}_\mathrm{ext}\right]_\mathrm{horizontal}=0 \quad \Rightarrow \quad }[/math] CONSTANT horizontal linear momentum (LM) relative to the ground!
Before stopping the block, the LM relative to the ground is associated only with the block: [math]\displaystyle{ (\leftarrow \ms\vs_0) }[/math]. But just after [math]\displaystyle{ (\ts_\mathrm{final}) }[/math], since the person and the block are at rest relative to the wagon, the entire system moves with the same velocity relative to the ground:[math]\displaystyle{ \left[\leftarrow (\Ms+\ms)\vs \right]. }[/math]. The conservation of horizontal LM between these two time instants allows the calculation of the final velocity of the system: [math]\displaystyle{ (\leftarrow \ms\vs_0) = \left[\leftarrow (\Ms+\ms)\vs \right] \quad \Rightarrow \quad \vs=\frac{\ms}{\Ms+\ms}\vs_0. }[/math].
ExD8-2-2-eng.png
The LM of just the block relative to the ground does not remain constant because of the friction force of the wagon on the block, which tends to stop it. For a time instant between the initial and final ones [math]\displaystyle{ (\ts_\mathrm{initial}\lt \ts\lt \ts_\mathrm{final}) }[/math] when the speed of the block relative to the ground has been reduced to [math]\displaystyle{ \vs'(\lt \vs_0) }[/math], the velocity of the system (person + wagon) can be calculated through the conservation of horizontal LM for the system (person + wagon with wheels + block):
[math]\displaystyle{ (\leftarrow \ms\vs_0) = (\leftarrow \ms\vs') + \left[\leftarrow (\Ms+\ms)\vs'' \right] \quad \Rightarrow \quad \vs''=\frac{\ms}{\Ms+\ms}(\vs_0-\vs'). }[/math]
ExD8-2-3-eng.png
ANIMACIONS

✏️ EXAMPLE D8.3: skater on ice


ExD8-3-1-neut.png
A person is skating on an ice rink. At a certain moment, his arms are symmetrically wide open and he he spins with angular velocity [math]\displaystyle{ \Omega_0 }[/math] In that configuration, the vertical axis through [math]\displaystyle{ \Gs }[/math] is a principal axis of inertia and the corresponding moment of inertia is [math]\displaystyle{ \Is_0 }[/math]. We want to investigate the evolution of the rotation when the configuration of his arms changes assuming that the friction between the ice and the skates is negligible [math]\displaystyle{ \mu=0 }[/math].
ExD8-3-2-neut.png
Is the angular momentum conserved?.
Since [math]\displaystyle{ \mu=0 }[/math] between ice and kates, the only external forces on the system (person + skates) are vertical (the weight and the normal forces of the ice on the skates). Those vertical forces cannot generate vertical momento about [math]\displaystyle{ \Gs }[/math]. Hence, for the system (person + skates):
[math]\displaystyle{ \left.\sum\overline{\Ms_\mathrm{ext}}(\Gs)\right]_\mathrm{vertical}=0=\left.\dot{\overline{\Hs}}_\mathrm{RTG}(\Gs)\right]_\mathrm{vertical} \quad \Rightarrow \quad \left.\overline{\Hs}_\mathrm{RTG}(\Gs)\right]_\mathrm{vertical} \text{CONSTANT!} }[/math]


The vertical angular momentum in the initial configuration is [math]\displaystyle{ \overline{\Hs}_\mathrm{RTG}(\Gs,\ts_\mathrm{initial})=(\Uparrow \Is_0 \Omega_0) }[/math]. When approachng or separating the arms from the trunk, the inertia moment of the person about the vertical axis through [math]\displaystyle{ \Gs }[/math] changes. For any value [math]\displaystyle{ \Is }[/math] of this inertia moment, conservation implies: [math]\displaystyle{ (\Uparrow \Is_0 \Omega_0)=(\Uparrow \Is \Omega) }[/math]. When approaching the arms to the trunk, [math]\displaystyle{ \Is\lt \Is_0 }[/math], therefore [math]\displaystyle{ \Omega\gt \Omega_0 }[/math] (the angular velocity increases). For the paricular case [math]\displaystyle{ \Is=\Is_0/2 }[/math], the angular velocity becomes twice the initial value: [math]\displaystyle{ \Omega=2\Omega_0 }[/math].
ANIMACIONS

✏️ EXAMPLE D8.4: collision between two bars


ExD8-4-1-eng.png
Two bars, with their mass concentrated at one end, move on a perfectly smooth horizontal ground (the friction coefficient between the ground and the bars is zero, [math]\displaystyle{ \mu=0 }[/math]) towards each other until they collide and become stuck. We want to describe the final motion of the system.
Is the linear momentum conserved?.
If we consider the system formed by the two bars, the external forces on them are strictly vertical (perpendicular to the plane of motion): the weight and the normal forces associated with the ground contact. Therefore, for this system:
[math]\displaystyle{ \left.\sum \overline{\Fs}_\mathrm{ext}\right]_\mathrm{horizontal}=0 \quad \Rightarrow \quad }[/math] CONSTANT horizontal linear momentum (LM) relative to the ground!
Before collision [math]\displaystyle{ (\ts_\mathrm{before}) }[/math]:
[math]\displaystyle{ \left.\overline{\mathrm{QM}}\right]_\mathrm{horizontal}=\Ms \vel{G}{T}=2\ms\overline{\vs}_\Ts(\mathrm{barra P})+\ms\overline{\vs}_\Ts(\mathrm{barra Q})=(\rightarrow \ms\vs_0)+(\leftarrow \ms2\vs_0)=0 }[/math]
After collision [math]\displaystyle{ \ts_\mathrm{after} }[/math], [math]\displaystyle{ \left.\overline{\mathrm{QM}}\right]_\mathrm{horizontal} }[/math] of the system has to be zero, therefore the velocity of the system’s center of inertia is also zero: [math]\displaystyle{ \overline{\vs}_\Ts(\Gs,\ts_\mathrm{after}) }[/math]. Hence, after collision, the rigid body formed by the two bars will have the ICR relative to the ground permanently located at [math]\displaystyle{ \Gs }[/math]:
ExD8-4-2-eng.png
Position of the inertia center [math]\displaystyle{ \Gs }[/math]: on the line [math]\displaystyle{ \Ps }[/math] and [math]\displaystyle{ \Qs }[/math], at a distance 4L below [math]\displaystyle{ \Qs }[/math].
[math]\displaystyle{ \left.\QGvec\right]_{\uparrow \downarrow}=\frac{\left.\ms \QQvec \right]_{\uparrow \downarrow} +\left. 2\ms \QPvec\right]_{\uparrow \downarrow}}{\ms+2\ms} }[/math]
[math]\displaystyle{ \left.\QGvec\right]_{\uparrow \downarrow}=\frac{2}{3}(\downarrow 6\Ls)=(\downarrow 4\Ls) }[/math]
There is no conservation of the linear momentum for each bar separately: the collision generates very intense forces between them and perpendicular to the bars, that provoke nonzero acceleration of their inertia centres.
Is the angular momentum conserved?
On the other hand, vertical forces (perpendicular to the plane of motion) cannot generate vertical moments about any point. If we apply the AMT at [math]\displaystyle{ \Gs }[/math] to the system formed by the two bars:
[math]\displaystyle{ \left.\sum\overline{\Ms_\mathrm{ext}}(\Gs)\right]_\mathrm{vertical}=0=\left.\dot{\overline{\Hs}}_\mathrm{RTG}(\Gs)\right]_\mathrm{vertical} \quad \Rightarrow \quad \left.\overline{\Hs}_\mathrm{RTG}(\Gs)\right]_\mathrm{vertical} \text{CONSTANT!} }[/math]
[math]\displaystyle{ \left.\overline{\Hs}_\mathrm{RTG}(\Gs,\ts_\mathrm{before})\right]_\mathrm{vertical}=\left.\overline{\Hs}_\mathrm{RTG}(\Gs,\ts_\mathrm{after})\right]_\mathrm{vertical} }[/math]
At time [math]\displaystyle{ \ts_\mathrm{before} }[/math], the two bars have a translational motion, and therefore [math]\displaystyle{ \Gs }[/math] does not belong kinematically to either of them. Its angular momentum has to be calculated through barycentric decomposition . Taking into account that the center of inertia of bar P is [math]\displaystyle{ \Ps }[/math], and that of bar Q is [math]\displaystyle{ \Qs }[/math]:
[math]\displaystyle{ \overline{\Hs}_\mathrm{RTG}(\Gs,\ts_\mathrm{before})=\left.\overline{\Hs}_\mathrm{RTG}(\Gs,\ts_\mathrm{before})\right]_\mathrm{barP}+\left.\overline{\Hs}_\mathrm{RTG}(\Gs,\ts_\mathrm{before})\right]_\mathrm{barQ}= }[/math]
[math]\displaystyle{ \hspace{2.9cm}=\left.\overline{\Hs}_\mathrm{RTP}(\Ps,\ts_\mathrm{before}) \right]_\mathrm{barP}+\GPvec\times 2\ms\vel{P}{RTG}+\left.\overline{\Hs}_\mathrm{RTQ}(\Qs,\ts_\mathrm{before})\right]_\mathrm{barQ}+\GQvec \times 2\ms\vel{Q}{RTG}= }[/math]
[math]\displaystyle{ \hspace{2.9cm}=\Is_\mathrm{P}\velang{barP}{RTG} + \GPvec \times 2\ms\vel{P}{RTG}+\Is_\mathrm{Q}\velang{barQ}{RTG}+\GQvec\times 2\ms\vel{Q}{RTG} }[/math]
[math]\displaystyle{ \velang{barP}{RTG}=\velang{barQ}{RTG}=\vec{0} \quad \Rightarrow \quad \overline{\Hs}_\mathrm{RTG}(\Gs,\ts_\mathrm{before})=(\downarrow 2\Ls)\times 2\ms(\rightarrow \vs_0)+(\uparrow 4\Ls)\times \ms (\leftarrow 2\vs_0)=(\otimes 10\ms\vs_0\Ls) }[/math]
After collision, [math]\displaystyle{ \Gs }[/math] is a point fixed to the rigid body formed by the two bars stuck together. Therefore:
[math]\displaystyle{ \overline{\Hs}_\mathrm{RTG}(\Gs,\ts_\mathrm{after})= \Is_\mathrm{G}\velang{}{RTG}=\left[2\ms(2\Ls)^2+\ms(4\Ls)^2\right](\otimes \Omega_\mathrm{T})=(\otimes 24\ms\Ls^2\Omega_\mathrm{T}) }[/math]
Finally: [math]\displaystyle{ (\otimes 10\ms\Ls\vs_0)=(\otimes\ms\Ls^2\Omega_\mathrm{T})\quad \Rightarrow \quad \Omega_\mathrm{T}=\frac{5}{12}\frac{\vs_0}{\Ls} }[/math] .


Important comment
Although, for the system formed by the two bars, the vertical external moment is zero for any point, the angular momentum is not conserved either at [math]\displaystyle{ \Ps }[/math] or at [math]\displaystyle{ \Qs }[/math] because the two points are accelerated (their velocities change abruptly when the collision occurs):
[math]\displaystyle{ \acc{P}{Gal}=\frac{\Delta \vel{P}{Gal}}{\ts_\mathrm{after}-\ts_\mathrm{before}}=\frac{\left[\rightarrow (\vs_0-2\Ls\Omega_\mathrm{T})\right]}{\ts_\mathrm{after}-\ts_\mathrm{before}} }[/math] , [math]\displaystyle{ \acc{Q}{Gal}=\frac{\Delta \vel{Q}{Gal}}{\ts_\mathrm{after}-\ts_\mathrm{before}}=\frac{\left[\rightarrow (2\vs_0-4\Ls\Omega_\mathrm{T})\right]}{\ts_\mathrm{after}-\ts_\mathrm{before}} }[/math] .
Therefore:
[math]\displaystyle{ \left.\sum\overline{\Ms_\mathrm{ext}}(\Ps)\right]_\mathrm{vertical}+ \left.\PGvec \times \ms \acc{P}{Gal}\right]_\mathrm{vertical}=\left.\dot{\overline{\Hs}}_\mathrm{RTP}(\Ps)\right]_\mathrm{vertical} }[/math]
[math]\displaystyle{ (\uparrow 2\Ls)\times \ms \frac{\left[\rightarrow (\vs_0-2\Ls\Omega_\mathrm{T})\right]}{\ts_\mathrm{after}-\ts_\mathrm{before}} =\left[\otimes \frac{2\ms\Ls(\vs_0-2\Ls\Omega_\mathrm{T})}{\ts_\mathrm{after}-\ts_\mathrm{before}} \right]=\left.\dot{\overline{\Hs}}_\mathrm{RTP}(\Ps)\right]_\mathrm{vertical} \quad \Rightarrow \quad \left.\overline{\Hs}_\mathrm{RTP}(\Ps)\right]_\mathrm{vertical}\neq \text{constant} }[/math]


[math]\displaystyle{ \left.\sum\overline{\Ms_\mathrm{ext}}(\Qs)\right]_\mathrm{vertical}+ \left.\QGvec \times \ms \acc{Q}{Gal}\right]_\mathrm{vertical}=\left.\dot{\overline{\Hs}}_\mathrm{RTQ}(\Qs)\right]_\mathrm{vertical} }[/math]
[math]\displaystyle{ (\downarrow 4\Ls)\times \ms \frac{\left[\leftarrow (2\vs_0-4\Ls\Omega_\mathrm{T})\right]}{\ts_\mathrm{after}-\ts_\mathrm{before}} =\left[\otimes \frac{8\ms\Ls(\vs_0-2\Ls\Omega_\mathrm{T})}{\ts_\mathrm{after}-\ts_\mathrm{before}} \right]=\left.\dot{\overline{\Hs}}_\mathrm{RTQ}(\Qs)\right]_\mathrm{vertical} \quad \Rightarrow \quad \left.\overline{\Hs}_\mathrm{RTQ}(\Qs)\right]_\mathrm{vertical}\neq \text{constant} }[/math]


ANIMACIONS

✏️ EXAMPLE D8.5: collision of a ring and an articulated arm


ExD8-5-1-eng.png
The ring, with radius L and mass m, moves on a smooth horizontal ground with angular velocity [math]\displaystyle{ \Omega_0=\ns\vs_0/\Ls }[/math] relative to the ground (where n is an integer), and its centre [math]\displaystyle{ \Ps }[/math] approaches the end [math]\displaystyle{ \Qs }[/math] of the arm with velocity [math]\displaystyle{ \vs_0 }[/math]. The arm has a length 2L and a mass M, is articulated at point [math]\displaystyle{ \Os }[/math] fixed to the ground and is initially at rest. Because of the collision, the ring and arm stick together. The friction associated with the joint at [math]\displaystyle{ \Os }[/math] is neglected. We want to investigate the motion of the system after the collision.
Is the linear momentum conserved?.
The linear momentum of each element separately (ring and arm) is not conserved: the collision generates very intense horizontal forces between them that cause acceleration in their centers of inertia. In addition, the arm undergoes an intense force at the [math]\displaystyle{ \Os }[/math]-joint.
There is no conservation of the linear momentum for the system (ring + arm) either: the [math]\displaystyle{ \Os }[/math]-joint introduces forces into the plane of motion responsible for the acceleration of the system’s center of inertia [math]\displaystyle{ \Gs }[/math].
Is the angular momentum conserved?
ExD8-5-2-eng.png
For the system (ring + arm), the forces associated with the joint yield a nonzero vertical external moment (orthogonal to the plane of motion) at any point except at [math]\displaystyle{ \Os }[/math]:
[math]\displaystyle{ \left.\sum\overline{\Ms_\mathrm{ext}}(\Os)\right]_\mathrm{vertical}=0=\left.\dot{\overline{\Hs}}_\mathrm{RTG}(\Os)\right]_\mathrm{vertical} \quad \Rightarrow \quad \left.\overline{\Hs}_\mathrm{RTG}(\Os)\right]_\mathrm{vertical} \text{CONSTANT!} }[/math]
Since [math]\displaystyle{ \Os }[/math] is permanently fixed to the ground, it must be the permanent ICR relative to the ground of the rigid formed by the ring and the arm stuck together after the collision. Before the collision, the ring ICR is located at [math]\displaystyle{ \Ls/2 }[/math] below the center [math]\displaystyle{ \Ps }[/math]:
[math]\displaystyle{ \vel{S}{T}=\vel{P}{T}+\velang{}{0}\times \PSvec = (\rightarrow \vs_0) + \left(\otimes \frac{\ns\vs_0}{\Ls}\right)\times (\downarrow \Ls)=\left[\leftarrow (\ns-1)\vs_0\right]. }[/math]
The distance e between [math]\displaystyle{ \Ps }[/math] and the ring ICR relative to the ground before collision can be found from:
[math]\displaystyle{ \left.\begin{array}{l} \left|\vel{P}{T}\right|=\vs_0=\es \Omega_0 \\ \left|\vel{S}{T}\right|=(\ns-1) \vs_0=(\Ls-\es) \Omega_0 \end{array}\right\} \Rightarrow \es=\frac{\Ls}{\ns} . }[/math]
A negative value for n means that the ICR is located at a distance e above [math]\displaystyle{ \Ps }[/math].
ExD8-5-3-eng.png
Before the collision [math]\displaystyle{ \ts_\mathrm{before} }[/math], [math]\displaystyle{ \Os }[/math] is not a point fixed to the ring in general (it is not its ICR). Its angular momentum has to be calculated thorugh barycentric decomposition . The initial angular momentum of the arm is zero because it does not move:
[math]\displaystyle{ \overline{\Hs}_\mathrm{RTO=T}(\Os,\ts_\mathrm{before})=\left.\overline{\Hs}_\mathrm{T}(\Os,\ts_\mathrm{before})\right]_\mathrm{anella}= \left.\overline{\Hs}_\mathrm{RTP}(\Ps,\ts_\mathrm{before})\right]_\mathrm{anella} + \OPvec \times 2\ms\vel{P}{T}= }[/math]
[math]\displaystyle{ \hspace{3.4cm}=\Is_\mathrm{P} \left(\otimes \frac{\ns\vs_0}{\Ls} \right) + \left(\downarrow 2\Ls \right)\times \ms\left(\rightarrow \vs_0 \right) = \left(\otimes \ms\Ls^2 \frac{\ns\vs_0}{\Ls}\right) + \left(\odot 2\ms\Ls\vs_0 \right) = \left[ \otimes (\ns-2)\ms\Ls\vs_0 \right] }[/math]
After the collision:
[math]\displaystyle{ \overline{\Hs}_\mathrm{RTO}(\Os,\ts_\mathrm{after})= \Is_\mathrm{O}\overline{\Omega}_\Ts=\left( \Is_\mathrm{O}^\mathrm{anella}+ \Is_\mathrm{O}^\mathrm{braç} \right) \overline{\Omega}_\Ts= \left( \Is_\mathrm{G}^\mathrm{anella}+ \Is_\mathrm{O}^{\mathrm{anella}\otimes}+\Is_\mathrm{O}^\mathrm{braç} \right) \overline{\Omega}_\Ts = \left[ \ms\Ls^2 + \ms(2\Ls)^2+ \frac{4}{3} \ms\Ls^2\right]\overline{\Omega}_\Ts }[/math]
[math]\displaystyle{ \left.\begin{array}{l} \bar{\mathrm{H}}_{\text {RTO }}\left(\Os, \mathrm{t}_{\text {after }}\right)=\left(\otimes \frac{19}{3} \ms\Ls^2 \Omega_{\mathrm{T}}\right) \\ \bar{\mathrm{H}}_{\text {RTO }}\left(\Os, \mathrm{t}_{\text {before }}\right)=\left[\otimes(\mathrm{n}-2) \mathrm{mLv}_0\right] \end{array}\right\} \Rightarrow \bar{\Omega}_{\mathrm{T}}=\left[\otimes(\mathrm{n}-2) \frac{19}{3} \frac{\mathrm{v}_0}{\mathrm{~L}}\right] }[/math]
For [math]\displaystyle{ n\gt 2 }[/math], the system rotation is clockwise. For [math]\displaystyle{ n\lt 2 }[/math], it is counterclockwise. For [math]\displaystyle{ n=2 }[/math], the system is at rest.
ANIMACIONS

✏️ EXAMPLE D8.6: free rigid body in space


ExD8-6-1-neut.png
The rigid body consists of two homogeneous plates, with the same mass and height but different widths, glued at point [math]\displaystyle{ \Os }[/math]. We want to investigate whether any dynamic magnitude is conserved when it is launched in the air. Aerodynamic interactions are neglected.
Hi ha conservació de la quantitat de moviment?.
El sòlid està sotmès a l’atracció gravitatòria terrestre com a única força externa. Per tant, la component vertical de la quantitat de moviment respecte del terra no es conserva, però les horitzontals sí..
Ja que la quantitat de moviment respecte del terra i la velocitat del centre d’inèrcia [math]\displaystyle{ \vel{G=O}{T} }[/math] són estrictament proporcionals, les components horitzontals de [math]\displaystyle{ \vel{G}{T} }[/math] es mantenen constants..
Hi ha conservació del moment cinètic?
El torsor gravitatori al centre de gravetat [math]\displaystyle{ \Gs }[/math] (que coincideix amb el centre d’inèrcia [math]\displaystyle{ \Os }[/math]) es redueix a una força resultant i cap moment. Per tant:
[math]\displaystyle{ \sum\overline{\mathrm{M}}_\mathrm{ext}(\Gs)=\overline{0}=\dot{\overline{\mathrm{H}}}_\mathrm{RTG} (\Gs) \quad \Rightarrow \quad \overline{\mathrm{H}}_\mathrm{RTG} (\Gs) \mathrm{CONSTANT!} }[/math]
Per al cas del sòlid que s’estudia: [math]\displaystyle{ \overline{\mathrm{H}}_\mathrm{RTG} (\Gs) = \Is\Is (\Gs) \velang{}{RTG} = \Is\Is (\Gs) \velang{}{T}. }[/math]
El moment cinètic i la velocitat angular no són proporcionals en general (només ho són quan la direcció de la velocitat angular és una direcció principal d’inèrcia per al centre d’inèrcia [math]\displaystyle{ \Gs }[/math] ), i la conservació del primer no implica la constància de la segona.
Avaluació qualitativa del tensor d’inèrcia
En tractar-se les dues plaques de sòlids plans simètrics:


[math]\displaystyle{ \left[\Is\Is(\Gs)\right]=\left[\Is\Is(\Gs)\right]_\text{placa inf} + \left[\Is\Is(\Gs)\right]_\text{placa sup.} = \diag{\Is_{11}}{\Is_{11} + \Is_{33}}{\Is_{33}}+ \diag{2\Is}{\Is}{\Is} , \text{ amb} \Is_{11}\lt \Is_{33}. }[/math]
Avaluació quantitativa del tensor d’inèrcia


[math]\displaystyle{ \left[\Is\Is(\Gs)\right]=\frac{1}{3} \ms\Ls^2 \diag{1}{1+4}{4}+\frac{1}{3} \ms\Ls^2 \diag{2}{1}{1}=\frac{1}{3} \ms\Ls^2 \diag{3}{6}{5} \equiv \diag{\Is_\mathrm{petit}}{\Is_\mathrm{gran}}{\Is_\mathrm{mitjà}} }[/math]
Les direccions 1, 2 i 3 són les direccions principals d’inèrcia per a [math]\displaystyle{ \Gs }[/math].
Cálcul del moment cinètic
[math]\displaystyle{ \left\{\overline{\mathrm{H}}_\mathrm{RTG} (\Gs)\right\}=\diag{\Is_\mathrm{petit}}{\Is_\mathrm{gran}}{\Is_\mathrm{mitjà}} \vector{\Omega_1}{\Omega_2}{\Omega_3}=\vector{\Is_\mathrm{petit}\Omega_1}{\Is_\mathrm{gran}\Omega_2}{\Is_\mathrm{mitjà}\Omega_3} }[/math],no és proporcional a [math]\displaystyle{ \velang{}{T} }[/math] en principi.
Si la velocitat angular inicial és exclusivament en una de les tres direccions (és a dir, si la seva direcció es principal d’inèrcia per a [math]\displaystyle{ \Gs }[/math]), llavors sí que hi ha proporcionalitat entre [math]\displaystyle{ \overline{\mathrm{H}}_\mathrm{RTG} (\Gs) }[/math] i [math]\displaystyle{ \velang{}{T} }[/math], i la conservació del primer implica la de la segona.


ANIMACIONS

✏️ Exemple D8.7: giroscopi


ExD8-7-1-eng.png
El sistema consta d’un disc homogeni, de massa m i radi r, que està articulat a un suport de massa negligible, i d’una forquilla que pot girar lliurement al voltant de l’eix vertical. Entre suport i forquilla hi ha un motor. El moment d’inèrcia del suport respecte de l’eix vertical que passa pel centre del disc és [math]\displaystyle{ \Is=(\lambda/2)\ms\rs^2 }[/math]. Inicialment [math]\displaystyle{ (\ts_\mathrm{incial} }[/math] el disc està paral·lel a terra, i gira amb velocitat angular vertical [math]\displaystyle{ \velang{disc}{T}=\psio }[/math] . Es negligeixen les friccions associades a totes les articulacions. Es tracta d’investigar com es mou el suport quan el motor canvia l’orientació del disc respecte del terra .
Hi ha conservació del moment cinètic?.
Per al SISTEMA disc, el moment total respecte del seu centre d’inèrcia [math]\displaystyle{ \Gs }[/math] és nul en la direcció del seu eix. El motor pot canviar l’orientació d’aquest eix respecte del terra (i respecte de qualsevol referència que es traslladi respecte del terra), i per tant no es tracta d’una direcció fixa al terra (per tant, tampoc a la RTG): no es conserva el moment cinètic en aquesta direcció.
Per al SISTEMA (disc + suport + forquilla), el moment total respecte del centre del disc [math]\displaystyle{ \Os }[/math] és nul en la direcció vertical, que sí que és fixa a terra. Per tant:
[math]\displaystyle{ \left.\sum \overline{\Ms}_\mathrm{ext}(\Os)\right]_\mathrm{vert} =0 \quad \Rightarrow \quad \left.\overline{\Hs}_\mathrm{RTO=T}(\Os) \right]_\mathrm{vert} \text{ CONSTANT!} }[/math]
Mentre el motor canvia l’orientació del pla del disc [math]\displaystyle{ (\dot{\theta} \neq 0) }[/math] , apareix la rotació del suport al voltant de l’eix vertical [math]\displaystyle{ \dot{\psi} }[/math] . El moment cinètic a [math]\displaystyle{ \Os }[/math] en cada instant és:
ExD8-7-2-neut.png
[math]\displaystyle{ \overline{\Hs}_\mathrm{RTO=T}(\Os,\ts)=\Is\Is^\mathrm{forq}(\Os)\velang{forq}{T}(\ts)+\Is\Is^\mathrm{disc}(\Os)\velang{disc}{T}(\ts)=\Is\Is^\mathrm{forq}(\Os)\dot{\psi}+\Is\Is^\mathrm{forq}(\Os)\left( \overline{\dot{\psi}}+ \overline{\dot{\theta}}+ \overline{\dot{\varphi}}\right) }[/math]


[math]\displaystyle{ \braq{\overline{\Hs}_\Ts^\mathrm{forq}(\Os,\ts)}{B}=\diag{\Is_{11}}{\Is_{22}}{(\lambda/2)\ms\rs^2}\vector{0}{0}{\dot{\psi}}=\vector{0}{0}{(\lambda/2)\ms\rs^2 \dot{\psi}}, }[/math]


[math]\displaystyle{ \braq{\overline{\Hs}_\Ts^\mathrm{disc}(\Os,\ts)}{B'}=\frac{1}{4}\ms\rs^2\diag{1}{1}{2}\vector{-\dot{\theta}}{-\dot{\psi} \sin\theta}{\dot{\varphi}+\dot{\psi}\cos\theta}=\frac{1}{4}\ms\rs^2\vector{-\dot{\theta}}{-\dot{\psi} \sin\theta}{2(\dot{\varphi}+\dot{\psi}\cos\theta)} }[/math]


El moment cinètic en direcció vertical prové de la projecció de les components 2 i 3:
[math]\displaystyle{ \left.\overline{\Hs}_\Ts(\Os,\ts)\right]_\mathrm{vert} =\overline{\Hs}_\Ts^\mathrm{sup}(\Os,\ts)+ \left.\overline{\Hs}_\Ts^ \mathrm{disc} (\Os,\ts) \right]_{3'}\cos\theta - \left.\overline{\Hs}_\Ts^\mathrm{disc}(\Os,\ts)\right]_{2'} \sin\theta , }[/math]
[math]\displaystyle{ \left.\overline{\Hs}_\Ts(\Os,\ts)\right]_\mathrm{vert} = \left(\Uparrow \frac{\lambda}{2}\ms\rs^2\dot{\psi}\right)+ \left(\Uparrow \frac{1}{4}\ms\rs^2\left[2\dot{\varphi}\cos\theta+\dot{\psi}(1+\cos^2\theta)\right]\right) }[/math]


Imposant la conservació de moment cinètic vertical:
[math]\displaystyle{ \left.\begin{array}{ll} \left.\overline{\mathrm{H}}_{\mathrm{T}}(\mathbf{O}, \mathrm{t})\right]_{\text {vert }}=\left(\Uparrow \frac{1}{4} \mathrm{mr}^2\left[2 \dot{\varphi} \cos \theta+\dot{\psi}\left(1+2 \lambda+\cos ^2 \theta\right)\right]\right) \\ \left.\begin{array}{l} \dot{\psi}\left(\mathrm{t}_{\text {inicial }}\right)=0 \\ \dot{\varphi}\left(\mathrm{t}_{\text {inicial }}\right)=\dot{\varphi}_0 \\ \theta\left(\mathrm{t}_{\text {inicial }}\right)=0 \end{array}\right\} \left.\Rightarrow \overline{\mathrm{H}}_{\mathrm{T}}\left(\mathbf{O}, \mathrm{t}_{\text {inicial }}\right)\right]_{\text {vert }}=\left[\Uparrow\left(\frac{1}{2} \mathrm{mr}^2 \dot{\varphi}_0\right)\right] \\ \end{array}\right\} \Rightarrow 2 \dot{\varphi} \cos \theta+\dot{\psi}\left(1+2 \lambda+\cos ^2 \theta\right)=2 \dot{\varphi}_0 }[/math]


Per altra banda, per al SISTEMA disc, el moment extern en la direcció de l’eix del disc (direcció 3’) és nul.
Per tant, [math]\displaystyle{ \left.\dot{\overline{\Hs}}_\mathrm{disc,T}(\Os)\right]_{3'}=0 }[/math]
[math]\displaystyle{ \braq{\dot{\overline{\Hs}}_\mathrm{disc,T}(\Os,\ts)}{B'}=\frac{1}{4}\ms\rs^2 \vector{-\ddot{\theta}}{-\ddot{\psi} \sin\theta -\dot{\psi}\dot{\theta}\cos\theta}{2(\ddot{\varphi}+\ddot{\psi}\cos\theta-\dot{\psi}\dot{\theta}\sin\theta)} + \vector{-\dot{\theta}}{-\dot{\psi}\sin\theta}{\dot{\psi}\cos\theta}\times\frac{1}{4}\ms\rs^2\vector{-\dot{\theta}}{-\dot{\psi}\sin\theta}{2(\dot{\varphi}+\dot{\psi}\cos\theta)}= }[/math]


[math]\displaystyle{ \hspace{2.5cm}= \frac{1}{4}\ms\rs^2\vector{-\ddot{\theta}-\dot{\psi}(2\dot{\varphi}+\dot{\psi}\cos\theta)\sin\theta}{-\ddot{\psi}\sin\theta + 2\dot{\theta}\dot{\varphi}}{2(\ddot{\varphi}+\ddot{\psi}\cos\theta-\dot{\psi}\dot{\theta}\sin\theta)} \Rightarrow \ddot{\varphi}+\ddot{\psi}\cos\theta-\dot{\psi}\dot{\theta}\sin\theta=0. }[/math]


ExD8-7-3D-neut.png
La integració d’aquesta equació condueix a: [math]\displaystyle{ \dot{\varphi}+\dot{\psi}\cos\theta=\dot{\varphi}_0 }[/math] , on [math]\displaystyle{ \dot{\varphi}_0 }[/math] és la constant d’integració, que es determina imposant les condicions inicials.
Combinant aquest resultat amb l’anterior:
[math]\displaystyle{ \left.\begin{array}{l} 2\dot{\varphi}\cos\theta+\dot{\psi}(1+2\lambda+\cos^2\theta )=2\dot{\varphi}_0\\ \dot{\varphi}+\dot{\psi}\cos\theta=\dot{\varphi}_0 \end{array}\right\} \Rightarrow \frac{\dot{\psi}}{\dot{\varphi}_0}=\frac{2(1-\cos\theta)}{2\lambda+\sin^2\theta} }[/math]


ExD8-7-3-2D-neut.png

✏️ Exemple D8.8: barra dins de guia llisa giratòria


ExD8-8-1-eng.png
La barra PQ, homogènia i de massa m, es mou mantenint els seus dos extrems dins d’una guia llisa [math]\displaystyle{ (\mu=0) }[/math] , de radi r i massa negligible, que pot girar lliurement al voltant de la direcció vertical. L’angle POQ és de [math]\displaystyle{ 120^o }[/math]. Es tracta de determinar l’equació del moviment per a la coordenada [math]\displaystyle{ \psi }[/math] . Es negligeix la rotació de la barra sobre el seu eix (rotació pròpia [math]\displaystyle{ \dot{\varphi} }[/math] ).
Hi ha conservació de la quantitat de moviment?.
Les forces externes sobre la barra no són nul·les: a més del pes, hi ha forces de la guia sobre la barra a [math]\displaystyle{ \Ps }[/math] i a [math]\displaystyle{ \Qs }[/math] que només tenen component normal (dirigida cap a [math]\displaystyle{ \Os }[/math]) i component perpendicular al pla de la guia. En total, doncs, la força externa resultant sobre la barra té components en les tres direccions de l’espai, i la quantitat de moviment no es conserva.
Si s’analitzen les forces externes sobre el SISTEMA (barra + guia), la conclusió és la mateixa: a més del pes de la barra, hi ha la força d’enllaç associada al coixinet entre terra i guia, que té tres components no nul·les en principi.
Hi ha conservació del moment cinètic?
Per al SISTEMA (barra + guia), el moment extern sobre qualsevol punt de l’eix de rotació de la guia (en particular, per al punt [math]\displaystyle{ \Os }[/math]) té component vertical nul·la (doncs el moment d’enllaç del coixinet en aquesta direcció és nul, i el pes no pot donar moment en direcció vertical). Per altra banda, l’acceleració angular de la guia respecte del terra [math]\displaystyle{ \left(\overline{\ddot{\psi}}\right) }[/math] té aquesta direcció. Per tant:
[math]\displaystyle{ \boxed{\left.\text{Full de ruta: SISTEMA (barra+guia), TMC a }\Os\right]_\mathrm{vert}} }[/math]


[math]\displaystyle{ \left.\sum\overline{\Ms}_\mathrm{ext}(\Os) \right]_\mathrm{vert}=0 \quad \Rightarrow \quad \left.\overline{\Hs}_\mathrm{RTG}(\Os)\right]_\mathrm{vert} \text{ CONSTANT!} }[/math]


L’únic element amb massa és la barra, i el punt [math]\displaystyle{ \Os }[/math] hi pertany cinemàticament :
ExD8-8-2-neut.png
[math]\displaystyle{ \overline{\Hs}_\mathrm{RTO}(\Os)=\Is\Is(\Os)\velang{barra}{RTO=T}=\left[\Is\Is(\Gs)+\Is\Is^\bigoplus(\Os)\right]\left(\overline{\dot{\psi}}+\overline{\dot{\theta}}\right) }[/math]


[math]\displaystyle{ \braq{\overline{\Hs}_\mathrm{RTO}(\Os)}{}=\left(\ms(\sqrt{3\rs})^2\diag{1}{0}{1}+\ms\left(\frac{\rs}{2}\right)^2\diag{1}{1}{0}\right)\vector{\dot{\theta}}{\dot{\psi}\sin\theta}{\dot{\psi}\cos\theta} }[/math]
[math]\displaystyle{ \braq{\overline{\Hs}_\mathrm{RTO}(\Os)}{}=\frac{1}{4}\ms\rs^2\vector{14\dot{\theta}}{\dot{\psi}\sin\theta}{13\dot{\psi}\cos\theta} }[/math]


[math]\displaystyle{ \left.\overline{\Hs}_\mathrm{RTO}(\Os)\right]_\mathrm{vert} =\left.\overline{\Hs}_\mathrm{RTO}(\Os)\right]_3\cos\theta+ \left.\overline{\Hs}_\mathrm{RTO}(\Os)\right]_2\sin\theta= \frac{1}{4}\ms\rs^2\dot{\psi}(13\cos^2\theta + \sin^2\theta)= \frac{1}{4}\ms\rs^2 \dot{\psi}(1+12\cos^2\theta) }[/math]
[math]\displaystyle{ \left.\overline{\Hs}_\mathrm{RTO}(\Os)\right]_\mathrm{vert} =\text{constant } \Rightarrow \quad \frac{\ds\left.\overline{\Hs}_\mathrm{RTO}(\Os)\right]_\mathrm{vert}}{\ds\ts}=0=\frac{1}{4}\ms\rs^2 \dot{\psi}(1+12\cos^2\theta)-6\ms\rs^2 \dot{\psi}\dot{\theta}\sin\theta\cos\theta }[/math]


[math]\displaystyle{ \boxed{\ddot{\psi}(3+7\cos^2\theta)-14\dot{\psi}\dot{\theta} \sin\theta \cos\theta =0} }[/math]


Comentari rellevant
ExD8-8-3-neut.png
El moment cinètic vertical no es conserva ni a [math]\displaystyle{ \Qs }[/math] ni a [math]\displaystyle{ \Ps }[/math] perquè tots dos punts estan accelerats:
[math]\displaystyle{ \sum \overline{\bar{\Ms}}_{\text {ext }}(\mathbf{Q})-\overline{\mathbf{P G}} \times \ms \overline{\mathrm{a}}_{\text {Gal }}(\mathbf{Q})=\dot{\overline{\mathrm{H}}}_{\text {RTQ }}(\mathbf{Q}), \quad \overline{\mathbf{QG}} \times \ms \overline{\mathrm{a}}_{\text {Gal }}(\mathbf{Q})=\overline{\mathbf{QG}} \times \mathrm{m}\left[\overline{\mathrm{a}}_{\text {RЕL }}(\mathbf{Q})+\overline{\mathrm{a}}_{\mathrm{ar}}(\mathbf{Q})+\overline{\mathrm{a}}_{\text {cor }}(\mathbf{Q})\right] }[/math]
[math]\displaystyle{ \left\{\overline{\mathbf{Q G}} \times \ms \bar{\mathrm{a}}_{\mathrm{Gal}}(\mathbf{Q})\right\}=\left\{\begin{array}{c} 0 \\ \sqrt{3\rs} \cos \theta \\ \sqrt{3\rs} \sin \theta \end{array}\right\} \times \ms\left[\left\{\begin{array}{c} 0 \\ \mathrm{a}_{\mathrm{REL}}^{\mathrm{s}} \sin \left(30^{\circ}-\theta\right)-\mathrm{a}_{\mathrm{REL}}^{\mathrm{n}} \cos \left(30^{\circ}-\theta\right) \\ \mathrm{a}_{\mathrm{REL}}^{\mathrm{s}} \cos \left(30^{\circ}-\theta\right)+\mathrm{a}_{\mathrm{REL}}^{\mathrm{n}} \sin \left(30^{\circ}-\theta\right) \end{array}\right\}+\left\{\begin{array}{c} \mathrm{a}_{\mathrm{ar}}^{\mathrm{s}}-\mathrm{a}_{\mathrm{Cor}} \\ -\mathrm{a}_{\mathrm{ar}}^{\mathrm{n}} \\ 0 \end{array}\right\}\right] }[/math]
[math]\displaystyle{ \left.\left.\left.\overline{\mathbf{Q G}} \times \ms \overline{\mathrm{a}}_{\text {Gal }}(\mathbf{Q})\right]_{\text {vert }}=\overline{\mathbf{QG}} \times \ms \overline{\mathrm{a}}_{\text {Gal }}(\mathbf{Q})\right]_{3^{\prime}}=\sqrt{3} \mathrm{m}\left(\mathrm{a}_{\text {Cor }}-\mathrm{a}_{\mathrm{ar}}^{\mathrm{s}}\right) \sin \theta \neq 0 \quad \Rightarrow \quad \dot{\bar{\Hs}}_{\text {RTQ }}(\mathbf{Q})\right]_{\text {vert }} \neq 0 }[/math]
[math]\displaystyle{ \mu=\text{datos.mean()} }[/math]
[math]\displaystyle{ \sigma=\text{datos.std()} }[/math]