Is Gravitational Attraction Negligible in Oscillating Systems?

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Homework Help Overview

The discussion revolves around the gravitational attraction in oscillating systems, particularly focusing on the forces acting on charges in a radial potential. Participants explore the implications of conservation laws and the nature of motion in a 1/r² potential, drawing parallels to classical mechanics and Kepler's laws.

Discussion Character

  • Mixed

Approaches and Questions Raised

  • Participants discuss various methods to analyze the forces on charges, including differential equations and conservation of energy and angular momentum. Questions about the nature of the forces, the role of centrifugal force, and the relationship between radial velocity and oscillation are raised.

Discussion Status

There is ongoing exploration of different interpretations of the problem, with some participants suggesting the use of Kepler's laws while others express confusion about the nature of the motion (ellipse vs. circular). Guidance has been provided regarding the application of conservation laws and the relationships between different variables, but no consensus has been reached.

Contextual Notes

Participants note the complexity of the problem, including the need to clarify the definitions of semi-major and semi-minor axes in the context of the charges' motion. There is also a recognition of the potential instability of the system being discussed.

Saitama
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Homework Statement


attachment.php?attachmentid=60257&stc=1&d=1373748865.png



Homework Equations





The Attempt at a Solution


I have tried to attack this problem with two methods but no luck. I always end up with something gibberish. :/

Method 1:
Considering the forces on anyone charge, the net force on a charge is -\frac{kq^2(3\sqrt{2}-4)}{4\sqrt{2}r^2}
hence,
ma=-\frac{kq^2(3\sqrt{2}-4)}{4\sqrt{2}r^2}
where ##a=\frac{d^2r}{dt^2}##, this leads to a differential equation of the form
\frac{d^2r}{dt^2}=-\frac{k}{r^2}
where k is some constant. Plugging this in wolfram alpha gives me nothing. :(

Method 2:
Throughout the motion, energy and angular momentum is conserved. The potential energy of charges at any instant is
-\frac{kq^2(3\sqrt{2}-4)}{\sqrt{2}r}
Let the velocity of charge along the radius vector be ##v_r## and perpendicular to radius vector is ##v_p##. Hence, the total kinetic energy is
4\left(\frac{1}{2}m(v_r^2+v_p^2)\right)
The total energy of the system at any time t is
E=-\frac{kq^2(3\sqrt{2}-4)}{\sqrt{2}r}+2m(v_r^2+v_p^2)
I don't really know what to do with this. Usually, in SHM problems, I would differentiate the expression for energy wrt time and set the derivative to zero but doing so here doesn't seem helpful. I can make one from equation from the fact that ##dL/dt=0## where L is the angular momentum of the system. L at any time is ##4mv_pr##. Even if I differentiate the expression for L, I will end up with an equation which doesn't look useful.

Any help is appreciated. Thanks!
 

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How did you get your equation for the force?

The motion in a 1/r^2-potential is called Kepler problem (he studied it for gravity), I guess you can use the formulas for that.It is amazing that such a system can exist (even if it is unstable).
 
My inclination is to solve the problem assuming L = constant = L0. The fact that the oscillations in L are not at all defined in terms of L(t) leads me to suspect that the net centripetal force on each +q charge is independent of L. That problem is pretty straight-forward.

However, I'm too lazy to prove that centripetal force is not a function of L.
 
mfb said:
How did you get your equation for the force?
That's the net force in the radial direction on a single charge. Do I have to consider the centrifugal force too? :rolleyes:
 
What happens to the radial velocity at the instants of maximum and minimum elongation of the sides of the square?
 
WannabeNewton said:
What happens to the radial velocity at the instants of maximum and minimum elongation of the sides of the square?

It becomes zero.
 
dr/dt = 0 when the sides are Lo or 1/4 Lo. Lo is given in the problem. Use conservation or energy and angular momentum for these configurations.

ehild
 
Pranav-Arora said:
It becomes zero.
Ok now use conservation law(s) for those instants. See where that takes you.

EDIT: darn it ehild. >.>
 
You were not present yet when I started to solve the problem and post. You were quicker, do it further.

ehild
 
  • #10
ehild said:
You were not present yet when I started to solve the problem and post. You were quicker, do it further.
It was a joke xD :smile: <3
 
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  • #11
ehild said:
dr/dt = 0 when the sides are Lo or 1/4 Lo. Lo is given in the problem. Use conservation or energy and angular momentum for these configurations.

ehild

$$E_i=-\frac{kq^2(3\sqrt{2}-4)}{L_0/4}+2mv_{pi}^2$$
$$E_f=-\frac{kq^2(3\sqrt{2}-4)}{L_0}+2mv_{pf}^2$$
Equating them
\frac{3kq^2(3\sqrt{2}-4)}{L_0}=2m(v_{pi}^2-v_{pf}^2)
Using conservation of angular momentum at these two instants,
4mv_{pi}\frac{L_0}{4\sqrt{2}}=4mv_{pf}\frac{L_0}{\sqrt{2}} \Rightarrow v_{pi}=4v_{pf}

Substituting the relation in energy in energy equation and solving for ##v_{pf}^2##,
v_{pf}^2=\frac{kq^2(3\sqrt{2}-4)}{10mL_0}

What should I do with this? :confused:
 
  • #12
Read the problem text again:-p

How are vpi and vpf related to the angular speed and Lo?

ehild
 
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  • #13
ehild said:
Read the problem text again:-p

ehild

I still don't get it. The problem asks the time period of oscillation but what I have is the square of final velocity. :confused:

##v_p## is the component of velocity perpendicular to the radius vector. ##v_{pi}## is the initial and ##v_{pf}## is the final.

##v_{pf}=\omega L_0/\sqrt{2}##?
 
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  • #14
Pranav-Arora said:
I still don't get it. The problem asks the time period of oscillation but what I have is the square of final velocity. :confused:

##v_p## is the component of velocity perpendicular to the radius vector. ##v_{pi}## is the initial and ##v_{pf}## is the final.

##v_{pf}=\omega L_0/\sqrt{2}##?

Yes, vpffL0/√2. So you know the maximum and minimum ω, but I have to think about the time period...

ehild
 
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  • #15
Pranav-Arora said:
Considering the forces on anyone charge, the net force on a charge is -\frac{kq^2(3\sqrt{2}-4)}{4\sqrt{2}r^2}

I agree with your expression for the force.

where ##a=\frac{d^2r}{dt^2}##

In polar coordinates, the radial acceleration is not \ddot{r} but rather ##\ddot{r}-r\dot{\theta}^2##.

The net force on a particle is an inverse square force. So, each particle travels an ellipse. I would follow mfb here. One of Kepler's laws should get you the answer straight away.
 
  • #16
TSny mentioned Kepler's 3rd law, so you could roll with that and get the answer in a direct fashion analogous to the case for gravitational interactions. Since you already got the final angular velocity ##\omega_{f}##, you could also use ##r^{2}_{f}\omega_{f} = \frac{2\pi}{P}ab## where ##P## is the period and ##a,b## are the semimajor and semiminor axes of the elliptical orbit (which you are given in the problem statement) of anyone of the charges respectively if you want: http://en.wikipedia.org/wiki/Kepler's_laws_of_planetary_motion#Second_law
 
  • #17
TSny said:
In polar coordinates...
2jb8imc.png

Is there no other way?
The net force on a particle is an inverse square force. So, each particle travels an ellipse. I would follow mfb here. One of Kepler's laws should get you the answer straight away.
Kepler's third law?
 
  • #18
WannabeNewton said:
TSny mentioned Kepler's 3rd law, so you could roll with that and get the answer in a direct fashion analogous to the case for gravitational interactions. Since you already got the final angular velocity ##\omega_{f}##, you could also use ##r^{2}_{f}\omega_{f} = \frac{2\pi}{P}ab## where ##P## is the period and ##a,b## are the semimajor and semiminor axes of the elliptical orbit of anyone of the charges respectively if you want: http://en.wikipedia.org/wiki/Kepler's_laws_of_planetary_motion#Second_law

How do I find a and b here? :confused:

Are they simply ##L_0/\sqrt{2}## and ##L_0/4\sqrt{2}##?
 
  • #19
The semimajor axis is the arithmetic average of the min and max position and the semiminor is the geometric average. I think it would be much easier to just go with what TSny said and just use Kepler's 3rd law. It's (Kepler's 3rd law) is usually written down in terms of the gravitational attraction but the potential here is essentially the same, just with different constants, so you would just have to adjust that part.

EDIT: By the way, by arithmetic average I meant ##a = (r_f + r_i) /2## and by geometric average I meant ##b = (r_f r_i)^{1/2}##
 
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  • #20
What is ##r_f## then? Is it equal to ##a##?
 
  • #21
Pranav-Arora said:
How do I find a and b here? :confused:

Are they simply ##L_0/\sqrt{2}## and ##L_0/4\sqrt{2}##?

No, those are not the lengths of the semi-major and semi-minor axes. They are the greatest and least distances to the central charge.
 
  • #22
TSny said:
No, they are not the lengths of the semi-major and semi-minor axes. They are the greatest and least distances to the central charge.

I am still confused. Why the path of the charges is an ellipse? Shouldn't they travel in a circle with a changing radius? This is how I analysed the situation before posting the problem here.
 
  • #23
What can be a circle with periodically changing radius? :)
 
  • #24
Pranav-Arora said:
I am still confused. Why the path of the charges is an ellipse? Shouldn't they travel in a circle with a changing radius? This is how I analysed the situation before posting the problem here.

A circle with a changing radius?

The motion of a particle acted on by an inverse square attractive force must be a conic section.
 
  • #25
Pranav-Arora said:
I am still confused. Why the path of the charges is an ellipse? Shouldn't they travel in a circle with a changing radius? This is how I analysed the situation before posting the problem here.
To put it another way, there is a maximum distance from the stationary charge that each of the orbiting charges reach and there is a minimum distance from the stationary charge that they reach. For the given potential, we can have an elliptic (which includes circular), parabolic, or hyperbolic trajectory. Here we have a periodic orbit with each charge having a maximum distance from the central chatge (apoapsis) and minimum distance from the central charge (periapsis) so we have an elliptical orbit.
 
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  • #26
From Kepler's third law
P^2 \propto a^3 \Rightarrow P^2=ka^3
where ##a=(L_0/\sqrt{2}+L_0/(4\sqrt{2}))/2=5L_0/(8\sqrt{2})## and k is some constant.

How should I determine k here? :confused:

I discussed a similar question before where I had to find this k. Please look at this thread: https://www.physicsforums.com/showthread.php?t=700759 (post #5) Can I use the same way here?
 
  • #27
Use the second law.
 
  • #28
ehild said:
Use the second law.

##a=5L_0/(8\sqrt{2})##, ##b=L_0/(2\sqrt{2})##
##r_f=L_0/\sqrt{2}##, ##\omega_f=\sqrt{2\times 10^3 (3\sqrt{2}-4)}##

Plugging them in ##r^{2}_{f}\omega_{f} = \frac{2\pi}{P}ab##
\frac{L_0^2}{4}\sqrt{2\times 10^3 (3\sqrt{2}-4)}=\frac{2\pi}{P}\frac{5L_0^2}{32}
Solving for P, ##P=0.178 sec##. Looks good?
 
  • #29
Pranav-Arora said:
That's the net force in the radial direction on a single charge. Do I have to consider the centrifugal force too? :rolleyes:
No centrifugal force. How did you arrive at those numbers?
 
  • #30
Pranav-Arora said:
##a=5L_0/(8\sqrt{2})##, ##b=L_0/(2\sqrt{2})##
##r_f=L_0/\sqrt{2}##, ##\omega_f=\sqrt{2\times 10^3 (3\sqrt{2}-4)}##

Plugging them in ##r^{2}_{f}\omega_{f} = \frac{2\pi}{P}ab##
\frac{L_0^2}{4}\sqrt{2\times 10^3 (3\sqrt{2}-4)}=\frac{2\pi}{P}\frac{5L_0^2}{32}
Solving for P, ##P=0.178 sec##. Looks good?

The area is correct. Show details of getting ωf. The formula for vpf in #11 was still correct.

ehild
 
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