Particle in Circular Motion: Newton's 2nd Law & Orbital Periods

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Homework Help Overview

The discussion revolves around a particle of mass m in circular motion, specifically analyzing the implications of Newton's second law and the relationship between angular velocity and orbital periods. The original poster seeks to demonstrate that the angular velocity remains constant and to establish a proportionality between the square of the orbital period and the cube of the orbital radius.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning, Assumption checking

Approaches and Questions Raised

  • Participants discuss the application of Newton's second law to derive relationships between angular velocity and orbital period. Questions arise regarding the identification of the proportionality constant and the appropriate formulas to use for calculations.

Discussion Status

Some participants have provided guidance on how to approach the problem, including references to Kepler's law and the relationship between period and radius. However, there is still uncertainty regarding the specific formulas and constants needed to proceed with the calculations.

Contextual Notes

Participants note the importance of understanding the definitions of terms such as the proportionality constant and the orbital period, as well as the implications of Newton's second law in the context of the problem. There is mention of missing information that may affect the approach to the question.

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The position of a particle of mass m moving in a circular orbit with radius r = ro is given by: r(t) = ro <er>

Show using Newton's second law of motion, that if the force responsible for this motion is given by:

F = -k/r^2 <er>

a) the angular velocity is constant in time, and
b) the square of the orbital period is proportional to the cube of the orbital radius. Compute the proportionality constant.

for far part a) L = |r x mv| = |mr^2(theta dot) <ez>|
therefore theta dot = L/mr^2

how do I start part b)?
 
Last edited:
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With the given proportionality, simply plug in any two points (ro and its corresponding To) and solve for the missing constant.
 
I forgot some parts of the question.

Now first off all, what is the proportionality constant?

And what is To?

What formula do I begin with?

Thanks
 
A proportionality constant is a constant such as k in Coloumb's law or G in Newton's law of gravitation. I guess its obvious now you didn't know, but the question is saying that the motion obeys Kepler's law (although you could've done it without knowing this), which takes the form:

[tex]T^2 = KR^3[/tex]

If you know the period and the radius of orbit, you can find K right?
 
K = (To^2)/(Ro^3)?

There is absolutely no way this question is that trivial. Remember I did forget to mention something in the question which had has now been in included, if it makes a difference.
 
How do I take into account Newton's second law F = -k/r^2 <er>?
 
To find part (a), the question probably wanted you to do:

[tex]F= \frac{k}{r^2} = m \omega^2 r[/tex]

In fact, by arranging this equation, you will be able to get the constant K.
 

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