- #36
Altabeh
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bcrowell said:Hi, Altabeh -- You and I don't seem to be convincing each other re g=2. Maybe it would help if Mentz114 or George Jones could take a look at this and give an opinion.
Here I take another approach to prove that if
[tex]\dot{t}=1/\sqrt{g_{tt}}=e^{-gy},[/tex]
then in the metric
[tex]d\tau^2=e^{2gy}dt^2-dy^2,[/tex]
particles following geodesics would give rise to a bizarre result which is only true if [tex]g=0[/tex]. (*)
But first off, I'd like to prove my velocity formula for the Rindler's metric
[tex]ds^2=e^{2\Phi}dt^2-dy^2,[/tex] (R)
in the case dealing with [tex]\Phi \propto y[/tex] where the proportionality constant is taken to be [tex]g[/tex].
If [tex]\Phi =gy[/tex], then obviously [tex](\Phi)' =g[/tex]. (Henceforth we denote the derivative wrt y by a prime and the derivative wrt proper time [tex]\tau[/tex] by a dot.)
We then write the geodesic equations in the Rindler's spacetime:
[tex] \ddot{y} + ge^{2gy}\dot{t}^2=0,[/tex] (1) and
[tex] \ddot{t} + 2g\dot{t}\dot{y}=0.[/tex] (2)
Re-write [tex]\ddot{y}[/tex] as
[tex]\ddot{y}=\dot{(\frac{dy}{dt}\frac{dt}{d\tau})}=\ddot{t}\frac{dy}{dt}+\dot{(\frac{dy}{dt})}\dot{t}.[/tex] (3)
Introducing (3) into (1) and making use of (2) gives
[tex]\ddot{y}=-2g\dot{t}\dot{y}\frac{dy}{dt}+\dot{(\frac{dy}{dt})}\dot{t}=-ge^{2gy}\dot{t}^2,[/tex] (V)
which can be written as
[tex]-2g{\dot{y}}^2+\dot{v}\dot{t}=-ge^{2gy}\dot{t}^2,[/tex]
in which [tex]v=dy/dt[/tex] represents the coordinate velocity. Now divide each side of this equation by [tex]\dot{t}^2:[/tex]
[tex]-2g(\frac{\dot{y}}{\dot{t}})^2+\frac{\dot{v}}{\dot{t}}=-ge^{2gy},[/tex]
and since [tex](\frac{\dot{y}}{\dot{t}})^2 = v^2[/tex] and [tex]a=\frac{\dot{v}}{\dot{t}}[/tex] representing the coordinate acceleration, we finally obtain
[tex]v^2=\frac{1}{2g}(a+ge^{2gy})[/tex] which is a generalized form of my velocity formula for [tex]g=1.[/tex]
It is time to say why a bizarre result would be reached if your assumption, bcrowell, holds using the Euler-Lagrange method: Divide each side of the metric (R) by [tex]d\tau^2:[/tex]
[tex](\frac{ds}{d\tau})^2=e^{2\Phi}\dot{t}^2-\dot{y}^2\equiv g_{\mu\nu}\dot{x}^{\mu}\dot{x}^{\nu}.[/tex]
You know that this must satisfy the Euler-Lagrange equations, i.e.
[tex]\frac{d}{d\tau}[\frac{\partial}{\partial \dot{x}^{\mu}}(g_{\mu\nu}\dot{x}^{\mu}\dot{x}^{\nu})]=\frac{\partial}{\partial {x}^{\mu}}(g_{\mu\nu}\dot{x}^{\mu}\dot{x}^{\nu}).[/tex]
So that for Rindler's metric (R) with [tex]\Phi = gy[/tex] we will have
[tex]\frac{d}{d\tau }(-2\dot{y})=2ge^{2gy}\dot{t}^2;[/tex]
[tex]\frac{d}{d\tau}(2\dot{t}e^{2gy})=0.[/tex]
A straightforward calculation confirms that these two are respectively given in (1) and (2). So assuming [tex]\dot{t}=1/\sqrt{g_{tt}}=e^{-gy}[/tex] and taking a dot derivative of it reveals that
[tex]\ddot{t}=-g\dot{y}e^{-gy}=-g\dot{y}\dot{t},[/tex] (4)
which is not abnormous iff particle is instantaneously at rest so [tex]\ddot{t}=0[/tex]. But instantaneously at rest means that proper acceleration would also vanish instantaneously, thus revealing
[tex]ge^{2gy}\dot{t}^2=0,[/tex]
from (1). This is again not abnormous iff g=0. (**) I think everything is now clear as sun: Demanding [tex]dy=0[/tex] costs so much for you because it does not let the proper acceleration be non-vanishing and consequently it does not preserve the non-flatness of spacetime.
AB
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(*) g is not 2 because I calculated geodesic equations based on a Rindler's metric with [tex]g=1[/tex] then worked your [tex]\dot{t}[/tex] into it to get [tex]g=2[/tex].
(**) This can be obtained from (V) as well. There you can see if [tex]v=a=0[/tex] inspired by your assumption, then [tex]g=0[/tex] necessarily.
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