1-dimensional problem in Newtonian gravity- HELP

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Discussion Overview

The discussion revolves around a one-dimensional problem in Newtonian gravity, specifically focusing on calculating the time it takes for a body to fall into the sun from a distance r, given the mass of the sun and the body. Participants explore various mathematical approaches and integrations related to this problem.

Discussion Character

  • Exploratory
  • Mathematical reasoning
  • Debate/contested

Main Points Raised

  • One participant presents the initial differential equation of motion for the body falling towards the sun and discusses difficulties in integrating it.
  • Another participant suggests using Kepler's law to relate the problem to a zero-width elliptical orbit, proposing a substitution for integration.
  • A different participant attempts to derive the time of fall using energy equations and presents a detailed integration process, expressing uncertainty about the validity of their approach.
  • Some participants acknowledge previous solutions found in related discussions, indicating that the problem has been addressed elsewhere.

Areas of Agreement / Disagreement

There is no consensus on the best approach to solve the problem, with multiple competing views and methods being discussed. Participants express uncertainty and explore different mathematical techniques without reaching a definitive solution.

Contextual Notes

The discussion includes complex integrations and substitutions that may depend on specific assumptions or definitions not fully resolved within the thread. Participants also indicate that previous discussions may contain relevant solutions, but these are not elaborated upon here.

Romeo
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1-dimensional problem in Newtonian gravity- HELP!

The problem is this:

Given sun of mass M and a body of mass m (M>>m) a distance r from the sun, find the time for the body to 'fall' into the sun (initially ignoring the radius of the sun).


Our first equation is therefore [tex]\frac {d^2r}{dt^2} = \ddot{r} = \frac {GM}{r^2}[/tex].

I am able to integrate this, giving:
[tex]\dot{r} = - {\sqrt{2GM}}{\sqrt{1/r - 1/R}}[/tex],

where R is the inital distance of the body from the sun. However, I am unable to integrate this again. I have shoved it into wolfram's integrator for an indicator of what to aim for, but cannot come close.

Any thoughts would be greatly appreciated.

Regards

Romeo
 
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You can think of this as a zero-width elliptical orbit, so you can use Kepler's law relating the orbital period to the length semi-major axis, and then take 1/4 of the orbital period of any orbit with the same semi-major axis.

If you insist on carrying out the integration, my textbook also suggests the substition

r = a(1-e*cos(psi))

in this case I think the eccentricity, e would be 1, so you'd have

r = a(1 - cos(psi))

I haven't tried this out, though.
 
Thank you pervect, it's an approach I hadn't considered.

Regards

Romeo
 
Aah, the triple post.
This has already been solved in Diff-eq.
 
Here is my try at it. Can you check for errors?
A rock is dropped from [tex]r_0[/tex] and falls straight down to R.
How long does it take. Where R is Earth radius and [tex]r_0 >> R[/tex].

The gravity force equation [tex]F= \frac{GMm}{r^2}[/tex] ,

integrates to a specific energy equation [tex]W= -\frac{u}{r}[/tex].

The velocity at some intermediate r is given by:

[tex]V=\sqrt{V_0^2+\frac{2u}{r} -\frac{2u}{r_0}}[/tex] .

This is a hard differential equation to solve for r(t). I believe I have a form which resembles your integral.

Change of symbols:

[tex]A=2u,\ \ \ \ B = -\frac{2u}{r_0},\ \ \ \ V_0=0[/tex]

[tex]V(r) = \sqrt{\frac{A}{r}+B}= \frac{dr}{dt}[/tex]

Now the part which I have never trusted.

[tex]\frac{dt}{dr}=\frac{1}{\sqrt{\frac{A}{r}+B}}[/tex]

Then [tex]\int_R^r dt= \int_\frac{A}{R}^\frac{A}{r} \frac{1}{\sqrt{\frac{A}{r}+B}}\ \ dr[/tex]

So [tex]T = \int_\frac{A}{R}^\frac{A}{r} \frac{1}{\sqrt{\frac{A}{r}+B}}\ \ dr[/tex]

A change of variables [tex]\frac{A}{r}=x,\ \ r=\frac{A}{x},\ \ dr=\frac{-A}{x^2}dx[/tex]

[tex] T = \int_\frac{A}{R}^\frac{A}{r} \frac{\frac{-A}{x^2}}{\sqrt{x+B}}\ \ dx = -A \left[ \frac{-\sqrt{B+x}}{Bx} -\frac{1}{2B} \left( \frac{2}{\sqrt{-B}} \arctan{ \sqrt{\frac{B+x}{-B}}} \right) \right]_\frac{A}{R}^\frac{A}{r}[/tex]

[tex]= \left[ \frac{-r_0 \sqrt{x-\frac{2u}{r_0}}}{x} -\frac{2r_0}{\sqrt{\frac{2u}{r_0}}} \arctan{\sqrt{\frac{x-\frac{2u}{r_0}}{\frac{2u}{r_0}}}} \right]_\frac{2u}{R}^\frac{2u}{r_0} =[/tex]

[tex]= \frac{-r_0 \sqrt{\frac{2u}{r_0}-\frac{2u}{r_0}}}{\frac{2u}{r_0}} -\sqrt{\frac{2}{u}} r_0^\frac{3}{2} \arctan{\sqrt{\frac{\frac{2u}{r_0}-\frac{2u}{r_0}}{\frac{2u}{r_0}}}} \ <br /> +\ \frac{r_0 \sqrt{\frac{2u}{R}-\frac{2u}{r_0}}}{\frac{2u}{R}} +\sqrt{\frac{2}{u}} r_0^\frac{3}{2} \arctan{\sqrt{\frac{\frac{2u}{R}-\frac{2u}{r_0}}{\frac{2u}{r_0}}}}[/tex]

[tex]= \frac{Rr_0}{\sqrt{2u}} \sqrt{\frac{1}{R}-\frac{1}{r_0}}+\sqrt{\frac{2}{u}} r_0^\frac{3}{2} \arctan{\sqrt{\frac{r_0}{R}-1}}= \sqrt{\frac{Rr_0}{2u}} \sqrt{r_0-R} +\sqrt{\frac{2}{u}} r_0^\frac{3}{2} \arctan{\sqrt{\frac{r_0}{R}-1}}[/tex]
This of course means you have to work the problem backwards usually as an iteration, but I would use a binary search which I found converges rapidly for the Kepler problem. It should be ok here too.
 
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