Orbits of planets/Angular momentum

  • Thread starter Thread starter Physics122
  • Start date Start date
  • Tags Tags
    Momentum Orbits
Click For Summary
SUMMARY

The discussion focuses on deriving the angular momentum (L) of an object in circular orbit around a mass (M) using fundamental physics principles. The key equations involved include L = r x mv and L = Iω, where r is the radius, m is the mass of the orbiting object, and ω is the angular velocity. Participants emphasize the relationship between gravitational force and centripetal force, leading to the conclusion that L can be expressed in terms of G, M, and the radius of the orbit. The derivation also touches on Kepler's laws and the proportionality of orbital period (P) to the average distance (A) raised to the 1.5 power.

PREREQUISITES
  • Newton's Law of Universal Gravitation
  • Centripetal Acceleration and Force
  • Angular Momentum and Angular Velocity
  • Kepler's Laws of Planetary Motion
NEXT STEPS
  • Explore the derivation of Kepler's Third Law (P = A^1.5)
  • Study the relationship between angular momentum and centripetal force
  • Learn about the implications of gravitational interactions in multi-body systems
  • Investigate the effects of varying orbital radius on angular momentum
USEFUL FOR

Students of physics, astrophysics enthusiasts, and anyone interested in understanding the dynamics of celestial orbits and angular momentum calculations.

Physics122
Messages
20
Reaction score
0

Homework Statement



Show that the angular momentum in circular orbit around a mass
M can be written as functions of just the masses, the
orbit radius, and G.


Homework Equations



L = r x p = r x mv
L = Iw


The Attempt at a Solution



I had no trouble showing that the total energy can be written with these variables, but the angular momentum is proving much tougher. I know this has to do with Keplars Law and maybe this will help:
Newton's law of universal gravitation states that the force is proportional to the inverse square of the distance; a_r = -GM/r^2
 
Physics news on Phys.org
Physics122 said:
I had no trouble showing that the total energy can be written with these variables, but the angular momentum is proving much tougher. I know this has to do with Keplars Law and maybe this will help:
Newton's law of universal gravitation states that the force is proportional to the inverse square of the distance; a_r = -GM/r^2

So far so good. Now think about how centripetal acceleration might fit into the picture too.
 
You also know that the acceleration is equal to the centripetal acceleration, v^2/r.
 
collinsmark said:
So far so good. Now think about how centripetal acceleration might fit into the picture too.

centripetal acceleration = force of gravity! (GMm/R^2)

bing bong boom do some calculations and convert the angular velocity from centripetal to velocity through v=wr and then I should get the angular momentum. One question, so
L=mvr and I found what v was and I already have r but to which mass does that m in the equation refer to??
 
No, centripetal acceleration = ACCELERATION of gravity. Remember that F=ma, so a force can never equal an acceleration.
 
ideasrule said:
No, centripetal acceleration = ACCELERATION of gravity. Remember that F=ma, so a force can never equal an acceleration.

oops sorry, I wrote out my thoughts too quickly, thusly they made no sense

Here was my thought process;

Fgrav = GMm/R^2
centripetal Force = mw^2R so I decided to set these two equal to each other and find the angular velocity which ended up being this:
w = the square root of (GMm/mR^3)
then keeping in mind that v=wR I get
v = R * the square root of (GMm/mR^3)
and because we know L = mvR I just plugged in the v I just got -->
L = m * (the square root of (GMm/mR^3) * R) * R

I really hope that's right because it makes sense to me. My only question was whether the beginning m was the orbiting object or the stationary one??
 
Seems right, but why didn't you cancel out the m's in GMm/mR^3?

"m" is the orbiting object's mass because centripetal (=towards center) force applies to the object that's moving in a circle.
 
Physics122 said:

Homework Statement



Show that the angular momentum in circular orbit around a mass
M can be written as functions of just the masses, the
orbit radius, and G.


Homework Equations



L = r x p = r x mv
L = Iw


The Attempt at a Solution



I had no trouble showing that the total energy can be written with these variables, but the angular momentum is proving much tougher. I know this has to do with Keplars Law and maybe this will help:
Newton's law of universal gravitation states that the force is proportional to the inverse square of the distance; a_r = -GM/r^2


Angular velocity is given as \omega, where \theta is the angle with some value, and \Delta is the change operator.

They have the given relationships:

\omega = \frac{\Delta \omega}{\Delta t}

\alpha = \frac{\Delta \omega}{\Delta t}

which reads that the angular acceleration is the change in angular velocity over time. Since you have the condition of L=I \omega, this means that we may as well describe this in terms of a linear momentum, without any perturbations.

It can be calculated that the velocity of the circular motion by the formula:

V_{constant} = \frac{2 \pi R^2}{t}
 
ideasrule said:
Seems right, but why didn't you cancel out the m's in GMm/mR^3?

"m" is the orbiting object's mass because centripetal (=towards center) force applies to the object that's moving in a circle.

In a similar vein, I was trying to figure out what would happen to the length of our days if the moons distance was 1.5 times its current value from earth. I found an equation online that said that P = A^1.5 where P is the orbital period and A is the average distance. I don't understand how they derived or got that equation? any ideas?
 
  • #10
Physics122 said:
In a similar vein, I was trying to figure out what would happen to the length of our days if the moons distance was 1.5 times its current value from earth. I found an equation online that said that P = A^1.5 where P is the orbital period and A is the average distance. I don't understand how they derived or got that equation? any ideas?

I wouldn't say that it's equal, but the period is proportional to distance raised to the 1.5 power, yes.

It can be derived with the same equations discussed in this thread. Just recognize that the period is time taken for the object to go all the way around the circle. In other words, the time taken for the object to traverse a distance of 2 \pi R. Noting that speed times time equals distance,

vP = 2 \pi R

or

P = \frac{2 \pi R}{v}

With that, combined with some other equations discussed in this thread, you should be able to calculate where the R1.5 proportionality comes from.
 
Last edited:
  • #11
collinsmark said:
I wouldn't say that it's equal, but the period is proportional to distance raised to the 1.5 power, yes.

It can be derived with the same equations discussed in this thread. Just recognize that the period is time taken for the object to go all the way around the circle. In other words, the time taken for the object to traverse a distance of 2 \pi R. Noting that speed times time equals distance,

vP = 2 \pi R

or

P = \frac{2 \pi R}{v}

With that, combined with some other equations discussed in this thread, you should be able to calculate where the R1.5 proportionality comes from.

I have just noticed I've used R^2 in my last post. This post has correctly stated the equation:

P = \frac{2 \pi R}{v} without any sqaure term - sorry about that. Glad no one noticed... i think ;)
 

Similar threads

  • · Replies 17 ·
Replies
17
Views
1K
  • · Replies 1 ·
Replies
1
Views
1K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 10 ·
Replies
10
Views
977
Replies
335
Views
16K
  • · Replies 7 ·
Replies
7
Views
3K
  • · Replies 7 ·
Replies
7
Views
8K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 6 ·
Replies
6
Views
2K
Replies
18
Views
7K