Crazy physics problem (big debate in my high school)

In summary, the conversation involves a problem of calculating the time taken for an object released from a distance of 10 Earth radii to reach the surface of Earth without considering the atmosphere. Different methods were suggested, such as using an energy approach or a differential equation, but there were discrepancies in the results. Some members also expressed their concerns about the level of expertise of certain science teachers.
  • #36
rohanprabhu said:
After a lot of battling with equations and a few mountain dews later.. I've arrived at a solution.. which i believe is quite correct. So.. i request you to please take a look and point out flaws [if any]:
<snip>

Putting it in the equation, we get the answer as:

[tex] r(t) = s\left(1 - \frac{1}{2e^{\Phi t}}\right) = s\left(1 - \frac{1}{2e^{\sqrt{2GM} t}}\right) [/tex]


This is the equation of motion I got. :D

I don't think this is correct- GM has units of L^3/T^2, so [tex]\sqrt{2GM}t[/tex] is not dimensionless. Not sure where the initial error occurs...
 
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  • #37
The integration looks wrong, in mathematica:

F[r_] = Expand[Integrate[(1/r - 1/s)^(-1/2), r]]

[tex]-\frac{1}{2} \tan ^{-1}\left(\frac{\sqrt{\frac{1}{r}-\frac{1}{s}} (2 r-s) \sqrt{s}}{2 (r-s)}\right) s^{3/2}-r \sqrt{\frac{1}{r}-\frac{1}{s}} s[/tex]
 
  • #38
Ok, people have tried excel, mathematica, maple...

I tried Python, pure and simple. No Runge-Kutta methods or anything, just pure dv = a*dt and dx = v*dt ...

I got the following results:

Final Velocity = 10607.0 m/s
Total Time Taken = 27943.16 seconds
Actual Final Velocity (from formula) = 10607.1 m/s

I think these confirm the earlier answers... I admit that trying to find the analytical solution is a much more interesting job ;)
 
  • #39
What about my effort on page 2? Anyone bother to go over that?
 
  • #40
I should've noticed it, gspeechc... I have been thinking along the exact same lines during the last hour. I'm too tired to develop it now, but I think that expression [ dx/ (lot of stuff) ] does have an anti derivative...

You made a mistake there, "x-10" should be replaced by x*10 (when cross multiplying R/x - 1/10) . I have been trying to get an expression substituting 10*R - x = z^2 (or -z^2 ... I haven't worked out the signs yet). Anyway, with such a subtitution, I find it becomes a solvable integral. Either that or I have made mistakes (more probable, that).
 
  • #41
In general,

[tex]
\Delta t = \int_{r_i}^{r_f}\frac{dr}{v(r)}
[/tex]

where [itex]r_i[/itex] and [itex]r_f[/itex] are the initial and final distances and [itex]v(r)[/itex] is the velocity (dr/dt) expressed as a function of r.

Combining conservation of energy and gravitational potential energy expressions yields an expression for velocity in terms of radial distance:

[tex]
v^2-v_0^2 = 2GM\left(\frac 1 r - \frac 1 {r_i}\right)
[/tex]

Here the velocity is negative (r is decreasing) until the object hits the Earth and the initial velocity is zero. Thus

[tex]
v = -\sqrt{2GM}\sqrt{\frac{r_i-r}{r \, r_i}}
[/tex]

Applying this result to the initial integral (note the change in integration order to accommodate the negative velocity):

[tex]
\Delta t = \frac 1 {\sqrt{2GM}} \int_{r_f}^{r_i}\sqrt{\frac{r \, r_i}{r_i-r}} \; dr
[/tex]

Using the the substitution [itex]r=r_i\sin^2\phi[/itex] ([itex]\phi = \sin^{-1}\surd{\frac r {r_i}}[/itex]) and defining [itex]\kappa\equiv r_f/r_i[/itex],

[tex]
\Delta t = \sqrt{\frac {r_i^3} {2GM}}
\int_{\sin^{-1}\surd{\kappa}}^{\pi/2}2\,\sin^2\phi \; d\phi
[/tex]

from which

[tex]
\Delta t = \sqrt{\frac {r_i^3} {2GM}}
\left(\sqrt{\kappa(1-\kappa)} + \cos^{-1}\surd{\kappa}\right)
[/tex]

With [itex]r_i=63781.37\,\text{km}[/itex], [itex]GM_e = 398600.4418\,\text{km}[/itex], and [itex]\kappa = 1/10[/itex], the above evaluates to 7.7628 hours = http://www.google.com/search?hl=en&...^2))*(sqrt(0.09)+acos(sqrt(0.1)))+in+seconds". (Link to Google calculator result highlighted)
 
Last edited by a moderator:
  • #42
D H said:
Combining conservation of energy and gravitational potential energy expressions yields an expression for velocity in terms of radial distance:

[tex]
v^2-v_0^2 = 2GM\left(\frac 1 r - \frac 1 {r_i}\right)
[/tex]

Here the velocity is negative (r is decreasing) until the object hits the Earth and the initial velocity is zero. Thus

[tex]
v = -\sqrt{2GM}\sqrt{\frac{r_i-r}{r \, r_i}}
[/tex]

absolute gem.. priceless. Great work!

and yes.. my method is wrong. The integration I did is wrong.. as pointed by a member in a previous post than this. Also, it is wrong for obvious reasons:

i] [itex]\sqrt{2GM}t[/itex] is used in exponentiation and is not dimensionless [pointed by Andy Resnick]
ii] The equation suggests that the object will gradually move slower.. whereas it should gradually move faster.

I did a really stupid mistake in my integration. While writing down.. i did not copy the 3/2 power and hence it came out as a simple equation derivate of Log[f[x]]...
 
Last edited:
  • #43
D H said:
In general,

[tex]
\Delta t = \int_{r_i}^{r_f}\frac{dr}{v(r)}
[/tex]

This equation seems pretty useful. Where's it derived from?
 
  • #44
awvvu said:
This equation seems pretty useful. Where's it derived from?

That is the 'definition' of velocity:

[tex]
v = \frac{dr}{dt}
[/tex]
 
  • #45
rohanprabhu said:
That is the 'definition' of velocity:

[tex]
v = \frac{dr}{dt}
[/tex]

Oh, doh.
 
  • #46
D H said:
[tex]
\Delta t = \sqrt{\frac {r_i^3} {2GM}}
\int_{\sin^{-1}\surd{\kappa}}^{\pi/2}2\,\sin^2\phi \; d\phi
[/tex]

from which

[tex]
\Delta t = \sqrt{\frac {r_i^3} {2GM}}
\left(\sqrt{\kappa(1-\kappa)} + \cos^{-1}\surd{\kappa}\right)
[/tex]

Just to stave off questions:

First, the parameter [itex]\phi[/itex] is obviously in the range[itex][0,\pi/2][/itex]. Phi starts at pi/2 at the release point and would drop to zero at the center of the Earth if the Earth's surface didn't stop the object first.

I integrated [itex]2\,\sin^2\phi[/itex] is done by the means of the identity [itex]2\,\sin^2\phi=1-\cos(2\,\phi)[/itex], yielding [itex]\phi-1/2\sin(2\,\phi)[/itex]. Evaluating wrt the limits leads to (phi part first) [itex]\pi/2-\sin^{-1}\surd\kappa[/itex]. This simplifies to [itex]\cos^{-1}\surd\kappa[/itex] via the [itex]\cos^{-1}x+sin^{-1}x = \pi/2[/itex]. To evaluate the sine term I used [itex]\cos(\sin^{-1}x) = \sqrt{1-x^2}[/itex] for [itex]x\in[0,\pi/2][/itex].
 
  • #47
I got it till the integration, and then made another substitution which didn't seem to yield a right answer... that teaches me to neglect trigonometric substitutions! ;)

That methods of yours really is a gem, DH. Especially the way you handled the phis and the kappas ;).
 
  • #48
rahuldandekar said:
That methods of yours really is a gem, DH. Especially the way you handled the phis and the kappas ;).

Thanks. 'Twas a fun little problem.
 

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