Two masses and spring oscillation

In summary, the question asks whether charging the masses with electric charges affects the oscillation period of an insulated spring and mass system. The correct approach is to use the concept of reduced mass and convert the two-body problem into a one-body problem, with the relative separation 'x' as the x-coordinate of the second mass. The differential equation for this problem is given by $\mu \frac{d^2 x}{dt^2} = -kx$, and for the charged masses, the electric force can be added and expanded to first order to find the effective spring constant. The correct approach is to use the concept of reduced mass and convert the two-body problem into a one-body problem, with the relative separation 'x' as the
  • #36
Tanya Sharma said:
I think I have confused myself by the usage of ‘x’ and xe .Initially I was using ‘x’ as extension in the spring and xe as equilibrium length of the spring .But as suggested by Vela in post#34 and by use of ehild in post#35 ,’x’ is being used as relative distance between the masses and xe as extension in the spring from its natural length at equilibrium .

No, I used x as you did x=x2-x1-L, , and xe is its value at equilibrium.
Tanya Sharma said:
The equilibrium length of the spring is xe+L .The separation between masses at any instant is x ,

No, the separation between masses is x+L.

But it would be less confusing to use x=x2-x1 as variable.

ehild
 
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  • #37
Tanya Sharma said:
The equilibrium length of the spring is xe+L .The separation between masses at any instant is x ,so extension in the spring from equilibrium length is given by x-(xe+L) .

Yes, this is confusing. You are taking xe to be the amount of stretch of the spring from its natural length at the equilibrium position. But then you take x to be the separation between the masses. So, your xe is not the equilibrium value of x.

If you take x to be the separation between the masses, then it would be natural to take xe to be the separation between the masses in the equilibrium position.

With x defined as the separation between the masses, write the equation of motion in terms of x and L.

Then let s, say, represent displacement from equilibrium: s = x - xe. (Here, xe is the value of x at equilibrium.)

s is assumed "small". Rewrite the equation of motion in terms of s and approximate it to first order in s.
 
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  • #38
TSny said:
Yes, this is confusing. You are taking xe to be the amount of stretch of the spring from its natural length at the equilibrium position. But then you take x to be the separation between the masses. So, your xe is not the equilibrium value of x.

If you take x to be the separation between the masses, then it would be natural to take xe to be the separation between the masses in the equilibrium position.

With x defined as the separation between the masses, write the equation of motion in terms of x and L.

Then let s, say, represent displacement from equilibrium: s = x - xe. (Here, xe is the value of x at equilibrium.)

s is assumed "small". Rewrite the equation of motion in terms of s and approximate it to first order in s.

$$ \mu \frac{d^2 x}{dt^2} = -k(x-x_e) + k_e\frac{q^2}{x^2} $$

$$ \mu \frac{d^2 s}{dt^2} = -ks + k_e\frac{q^2}{(s+x_e)^2} $$

Equilibrium condition is given by ## \frac{k_e q^2}{(x_e)^2} = k(x_e-L)##

Does it make sense ?
 
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  • #39
Tanya Sharma said:
$$ \mu \frac{d^2 x}{dt^2} = -k(x-x_e) + k_e\frac{q^2}{x^2} $$

$$ \mu \frac{d^2 s}{dt^2} = -ks + k_e\frac{q^2}{(s+x_e)^2} $$

Your expression for the spring force in these two equations is incorrect. When x = xe, there is a nonzero spring force balancing the electric force.
 
  • #40
Tanya Sharma said:
$$ \mu \frac{d^2 x}{dt^2} = -k(x-x_e) + k_e\frac{q^2}{x^2} $$

xe is not the same as the relaxed length of the spring. You equation should be $$ \mu \frac{d^2 x}{dt^2} = -k(x-L) + k_e\frac{q^2}{x^2} $$

Equilibrium means that distance between the masses when the net force is zero between them.
$$ 0 = -k(x_e-L) + k_e\frac{q^2}{x_e^2} $$

ehild
 
  • #41
See attached graph. Fs is the spring force, Fe is the electric force, F is the resultant.

ehild
 

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  • #42
$$ \mu \frac{d^2 x}{dt^2} = -k(x-L) + k_e\frac{q^2}{x^2} $$

$$ \mu \frac{d^2 s}{dt^2} = -k(s+x_e-L) + k_e\frac{q^2}{(s+x_e)^2} $$

Equilibrium condition is given by ## \frac{k_e q^2}{(x_e)^2} = k(x_e-L)##

Now let ##f(s) = k_e\frac{q^2}{(s+x_e)^2} ## .Taylor expanding the function about 0 ,we have f(s) = f(0)+f'(0)s

$$ f(0) = k_e\frac{q^2}{x_e^2} $$

$$ f'(0) = -2k_e\frac{q^2}{x_e^3}$$

$$ f(s) = k_e\frac{q^2}{(x_e)^2}-2k_e\frac{q^2}{(x_e)^3}s$$

$$ \mu \frac{d^2 s}{dt^2} = -ks -kx_e + kL+ k_e\frac{q^2}{(x_e)^2}-2k_e\frac{q^2}{(x_e)^3}s $$

$$ \mu \frac{d^2 s}{dt^2} + (k+2k_e\frac{q^2}{x_e^3})s = k_e\frac{q^2}{(x_e)^2} -kx_e+kL $$

Or, $$ \mu \frac{d^2 s}{dt^2} + (k+2k_e\frac{q^2}{x_e^3})s = 0 $$

Is it correct ?

Please say yes :shy:
 
  • #43
Tanya Sharma said:
Is it correct ?

Please say yes :shy:

Yes, that's correct!

Perhaps a bit shorter: The reduced-mass equation of motion has the form of a single particle of mass μ moving under a net force

F(x) = Fspring(x) + Felec(x).

Let xe be whatever value of x makes the net force zero.

Then, Taylor expand about xe:

F(x) ≈ F(xe) + F'(xe)(x-xe) = F'(xe)(x-xe) = F'(xe) s

Thus, -F'(xe) is the effective "spring constant".

[In ehild's graph, compare the slope of the blue curve at x = xe with the slope of the black line.]
 
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  • #44
Thank you so much ehild and TSny :) .
 
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  • #45
How can we do this problem using energy approach i.e conservation of energy ?

$$ E(x) = \frac{1}{2}k(x-L)^2+\frac{k_eq^2}{x}+\frac{1}{2}2mv^2 $$

Taking time derivative of the above equation and equating ## \frac{dE}{dt}=0 ##,we have

$$ k(x-L) \dot{x}- \frac{k_eq^2}{x^2} \dot{x}+2mv \dot{v} = 0 $$

Is it correct ? If yes ,how should I proceed ?
 
  • #46
You have to specify what is v and what is x, and how they are related. It is about small oscillations, but an isolated system can move as a whole and v can be anything. The kinetic energy need not be twice the KE of one mass.

ehild
 
  • #47
ehild said:
You have to specify what is v and what is x, and how they are related.

You are right .

'x' is the relative separation of the masses and 'v' is the speed of the masses w.r.t origin .

Should I write individual EOM for the masses or is it possible to write energy equation in terms of reduced mass ?

ehild said:
The kinetic energy need not be twice the KE of one mass.
ehild

Doesn't symmetry require the two masses to have equal speeds and since the COM is at rest ,the KE is double of the KE of an individual mass ?

What is the right way to approach using energy method?
 
  • #48
What symmetry do you speak about?
Where is the origin? In your first post you said it was to the left from m1. The CM is not in rest in arbitrary frames of reference.

If the origin is in the line connecting the masses, but arbitrary otherwise, and x=x2-x1, the KE is
[tex]KE=\frac{1}{2}(m_1x_1^2+m_2x_2^2)= \frac{1}{2}(m_1x_1^2+m_2(x+x_1)^2)[/tex]. In case m1=m2,
[tex]KE= \frac{1}{2}m(x_1^2+(x+x_1)^2)[/tex]
What do you do with x1?





ehild
 
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  • #49
$$ E(x) = \frac{1}{2}k(x_2 - x_1-L)^2+\frac{k_eq^2}{(x_2-x_1)}+\frac{1}{2}m_1\dot{x_1^2} +\frac{1}{2}m_2\dot{x_2^2} $$

Taking time derivative of the above equation and equating ## \frac{dE}{dt}=0 ##,we have

$$ k(x_2-x_1-L) (\dot{x_2}-\dot {x_1})- \frac{k_eq^2}{(x_2-x_1)^2 } (\dot{x_2}-\dot {x_1})+m_1\dot{x_1}\ddot{x_1} + m_2\dot{x_2}\ddot{x_2} = 0 $$

Does this make sense ?
 
  • #50
It is correct but of no use.
The energy is the first integral of the equation of motion. If you differentiate it you get back F=ma.
Choose a frame of reference first. If you assume the CM fixed, place the origin there. What does it mean to x1 and x2?

ehild
 
  • #51
OK...Please leave it for a while.

ehild said:
The potential consists of an elastic part and a Coulomb-part. Expand the potential function into Taylor series about the equilibrium point. Keep up to the second order term. From the equilibrium condition and from the coefficient of the second-order term, you get the equivalent force constant.

ehild

Could you show me how you would get the equivalent force constant using your above approach ?
 
  • #52
The second derivative of the potential is the negative of the first derivative of force. It would not be a different approach.
Anyway, you have to choose a frame-of reference first.

Sorry, I have to leave now, but I am soon back. ehild
 
  • #53
Congratulations on your 10000 post :smile:
 
  • #54
Thanks :smile: I did not notice. Back to equivalent force constant. The potential energy is a function of some variable x. Assume U(x) has a local extreme somewhere, at x0. You want to find the behaviour of the system near x0.
The Taylor series of a function f(x) about x0 is defined as

[tex]T(x)=\sum_0^∞{f^{n}|_{x=x_0}\frac{(x-x_0)^n}{n!}}[/tex]
where f(n) means the n-th derivative of f(x), and you have to take all derivatives at x=x0.

There are some criteria when you can do the expansion and the series converges to f(x).

Now we assume that U(x) can be expanded and we stop at the second-order term.

[tex]U(x)≈U(x_0)+\frac{df(x_0)}{dx} (x-x_0)+\frac{1}{2}\frac{d^2 f(x_0)}{dx^2}(x-x_0)^2[/tex]

f(x) has local extrem at x0, so the first derivative has to be zero. We can choose the zero of the potential energy at x0. Our approximate potential function reduces to one term [tex]U(x)≈\frac{1}{2}\frac{d^2 f(x_0)}{dx^2}(x-x_0)^2[/tex]

If the second derivative of the potential function is positive, it has a minimum at x0. The potential is the same as that of a spring, and the effective spring constant is equal to the second derivative of U at the equilibrium point.

[tex]D=\frac{d^2 f(x_0)}{dx^2}[/tex]

The force is negative gradient of the potential : F=-dU/dx = -D(x-x0)). You can switch over to the variable x-x0=s, and the the equation of motion is mds2/dt2+Ds=0. The angular frequency of the SHM is ω=√(D/m) (in our case, use the reduced mass).

ehild
 
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  • #55
I have a very basic question that when do we expand a function and keep terms up to first order term (i.e first two terms) just as in post #42 and when do we expand up to second order (i.e first three terms) just as in above post ?
 
  • #56
You can ignore the second order term in an expansion if it and all the other terms are much smaller than the first order one. If the first order-term is zero, as in the case at the bottom of a potential well, you have to keep the second order term.

How many terms are needed, it depends on the deviation from x0, the centre of the expansion.
In this problem, we were interested in small oscillation about an equilibrium position. |x-x0|could be sufficiently small.

ehild
 
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  • #57
ehild said:
You can ignore the second order term in an expansion if it and all the other terms are much smaller than the first order one. If the first order-term is zero, as in the case at the bottom of a potential well, you have to keep the second order term.

ehild

Okay...thanks for enlightening me :)

Another naive question

But what if the first order term is not present ?

What is approximate value of ##(1-(\frac{d}{x})^2)^2## under the assumption x<<d ? Should it be ##1## or should it be ## 1-2(\frac{d}{x})^2 ## ?
 
  • #58
Tanya Sharma said:
Okay...thanks for enlightening me :)

Another naive question

But what if the first order term is not present ?

What is approximate value of ##(1-(\frac{d}{x})^2)^2## under the assumption x<<d ? Should it be ##1## or should it be ## 1-2(\frac{d}{x})^2 ## ?

If the first term is not present expand to the second-order term.

Remember cosx. If x is small, usually it is approximated by 1 or by 1-x2.

##(1-(\frac{d}{x})^2)^2## under the assumption x<<d : if x<<d then d/x >> 1 and you can ignore 1.

If you mean (1-(x/d)2)2 it is approximately 1-2(x/d)2.

But it depends what else is in the expression you want to approximate. If it is 1-(1-(x/d)2)2, you have to keep the second-order term. If it is 4+(1-(x/d)2)2, for example, you might ignore (x/d)2

ehild
 
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  • #59
I was initially hesitant (rather afraid) asking these questions .But after reading the explanations I am quite glad and very satisfied that I put my doubts in front of you .

Thanks ehild :smile:
 
  • #60
I read just now : "the only stupid question is which is not asked".:smile:

ehild
 
  • #61
Returning to your energy consideration, and assuming the CM is in rest: If you have two masses with coordinates x1 and x2 corresponding velocities v1 and v2, and you introduce the variable x=x2-x1, the corresponding velocity v=v2-v1:

CM is in rest: m1v1+m2v2=0, and v2-v1=v →
##v_1=-\frac{m_2v}{m_1+m_2}\\v_2=\frac{m_1v}{m_1+m_2}##

The kinetic energy is

##KE=\frac{1}{2} \left(m_1 (\frac{m_2 v}{m_1+m_2} )^2+ m_2( \frac{m_1 v}{m_1+m_2})^2 \right)##

##KE=\frac{1}{2}\frac{m_1 m_2}{m_1+m_2} v^2=\frac{1}{2} μ v^2##

Assuming SHM about the equilibrium value of x: x-xe=Asin(ωt), v=Aωsin(ωt) and expanding the potential energy about xe: PE=0.5 D(x-xe)2

KE+PE=E →

##\frac{1}{2} A^2\left((μω)^2\cos^2(ωt)+D^2 \sin^2(ωt)\right)=E##

The expression can be constant only when μω=D.
 
  • #62
Hello ehild

ehild said:
Here is the derivation how a two-body problem can be reduced to one body-problem. I write it in one dimension,but the derivation is the same for 3D.

I would like to understand how this concept of reduced mass is applied in case of a Planet of mass m moving around sun of mass M in circular orbit

Suppose the Sun is considered stationary .In that case ## \frac{GMm}{D^2}=\frac{mv^2}{D}## where D is the distance between them .This gives ##v=\sqrt{\frac{GM}{D}}##

Now if we want to take into account the motion of Sun also i.e both Sun and the planet orbiting about their common COM then this is equivalent to replacing the mass of planet 'm' by reduced mass 'μ = Mm/(M+m)' and replacing the Sun with a central mass 'M+m' .

Using this we have ## \frac{G(M+m)\mu}{D^2}=\frac{mv^2}{D}##

Solving we get ##v=\sqrt{\frac{GM}{D}}## .

I am wondering why hasn't the result changed since now the Sun is also considered to be orbiting ?
 
  • #63
What is v now?

ehild
 
  • #64
Speed of the planet in circular orbit.
 
  • #65
No. The reduced-mass approach started by introducing new variables instead of the position vectors of the planet and Sun. You might look at my post in this thread about it.

ehild
 
  • #66
Tanya Sharma said:
I would like to understand how this concept of reduced mass is applied in case of a Planet of mass m moving around sun of mass M in circular orbit

Suppose the Sun is considered stationary .In that case ## \frac{GMm}{D^2}=\frac{mv^2}{D}## where D is the distance between them .This gives ##v=\sqrt{\frac{GM}{D}}##
By assuming the Sun is stationary, you've reduced the two-body problem to a one-body problem. In this case, you're assuming the Sun doesn't move because its mass M is so much larger than the mass of the planet.

Using the reduced-mass approach instead, you get
$$\frac{GMm}{D^2} = \frac{\mu v^2}{D}.$$ The force between the two bodies remains unchanged, but the mass of moving body is replaced by the reduced mass ##\mu##. When ##M \gg m##, you have ##\mu \cong m##, and you recover the previous result.

Now if we want to take into account the motion of Sun also i.e both Sun and the planet orbiting about their common COM then this is equivalent to replacing the mass of planet 'm' by reduced mass 'μ = Mm/(M+m)' and replacing the Sun with a central mass 'M+m' .
I'm not sure how you came up with this.
 
  • #67
The two-body Kepler problem can be solved by using the CM mass of reference. The difference of the position vectors obey the same differential equation as a single body with the reduced mass orbiting about a stationary mass of m+M. The gravitational force between the mass and the planet is F= GmM/D2. That between the reduced mass and a central mass of m+M: G μ(M+m)/D2= G(mM/(m+M))(M+m)/D2=GmM/D2.

ehild
 
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  • #68
Ah, now I understand what Tanya was getting at in her post.

Tanya, you have a mistake in the equation of motion in the second approach, which is why you're ending up with identical results for ##v##. You have to replace ##m## by ##\mu## on the righthand side.
 
  • #69
vela said:
Ah, now I understand what Tanya was getting at in her post.

Tanya, you have a mistake in the equation of motion in the second approach, which is why you're ending up with identical results for ##v##. You have to replace ##m## by ##\mu## on the righthand side.

$$ \frac{G(M+m)\mu}{D^2}=\frac{\mu v^2}{D} $$

$$ v^2 = \frac{G(M+m)}{D} $$

$$ v = \sqrt{\frac{GM(1+\frac{m}{M})}{D}} $$

Now ,since ##m<<M## , neglecting term ##\frac{m}{M} ## , ## 1+\frac{m}{M} ≈ 1 ##

$$ v = \sqrt{\frac{GM}{D}} $$

But again this is the same result as before .
 
  • #70
Yes, that's correct. You see to that level of approximation, both approaches yield the same result, as you should expect. If you expand ##\sqrt{1+\frac mM}## as a series, you can calculate the higher-order corrections that come from relaxing the assumption that M is stationary.
 

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