Schwarzschild metric with angular momentum

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SUMMARY

The discussion focuses on the Schwarzschild metric generalization for a rotating mass M with angular momentum J, specifically addressing the conserved quantities E and L for a test particle in a stable circular orbit. The equations derived include E^2 = 1 - M/R and L = √(M R), which are obtained by analyzing the effective potential and the equations of motion in the equatorial plane. The participants explore the implications of these equations and the necessary approximations to derive the effective potential for the test particle.

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Homework Statement



Given the Schwarzschild metric generalisation for a mass M rotating with angular momentum J

##ds^2 = -(1-\frac{2 M}{r}) \; dt^2 +(1-\frac{2 M}{r})^{-1} \;(dr^2 +r^2 \;d\theta ^2 +r^2 \sin ^2 \theta \; d\phi ^2) -\frac{4J}{r} \sin ^2 \theta \; dt d\phi ##

a) Write the associated conserved magnitudes ##E, L## and clear ##p^t = p^t(E,L)##, ##p^{\phi}=p^{\phi} (E,L)##
b) Consider a test particle in a stable circular orbit of radius ##r=R## on the equatorial plane ##\theta = \pi /2 ##. Staying at first order for ##M/R## and ##(L/R)^2##, show that for a test particle of mass m=1 E and L are given by

##E^2=1-M/R##
##L=\sqrt{M R}##

Homework Equations



##E= - \vec{T} \cdot \vec{u}##
##L=\vec{R} \cdot \vec{u}##

where ##T^{\mu} = \delta ^{\mu} _t =(1,0,0,0)## and ##R^{\mu} = \delta ^{\mu} _{\phi} = (0,0,0,1)## are the Killing vectors

##u^{\mu} u_{\mu}= u^{\mu} g_{\mu \nu} u^{\nu} = -1##

The Attempt at a Solution


a)
Calling ##B(r)=(1-\frac{2 M}{r})##, the conserved quantities are

##E=-T^{\mu} g_{\mu \nu} u^{\nu} = -T^t g_{t t} u^t -T^t g_{t \phi} u^{\phi} = B(r) \dot{t} + \frac{2 J}{r} \sin ^2 \theta \; \dot{\phi} ##

##L= R^{\mu} g_{\mu \nu} u^{\nu} = R^{\phi} g_{\phi \phi} u^{\phi} + R^{\phi} g_{\phi t} u^t= B^{-1} (r) r^2 \sin ^2 \theta \; \dot{\phi} - \frac{2 J}{r} \sin ^2 \theta \; \dot{t} ##

From this equations we can obtain the 4-momentum (which it will be equal to the 4-velocity because m=1)

##\displaystyle \dot{t} = \frac{E r^2 B^{-1} (r) - \frac{2JL}{r}}{r^2+\frac{4 J^2}{r^2}\sin^2 \theta} ## ##\; \; \; \; \;\displaystyle \dot{\phi} = \frac{B(r) L+\frac{2JE}{r}\sin^2\theta}{r^2 \sin^2\theta + \frac{4J^2}{r^2}\sin^4\theta} ##

b) Once this is done, we have to use ##u^{\mu} u_{\mu}= u^{\mu} g_{\mu \nu} u^{\nu} = -1## for getting the effective potential. Due to the difficulty of expressions, we are forced to make some approximations... and here is my problem. How to make it? I tried (setting ##r=R## and ##\theta = \pi /2##)

##\displaystyle \dot{t} = \frac{ R^4 E B^{-1} - 2JLR}{R^4+4J^2} \approx \frac{ R^4 E B^{-1} - 2JLR}{R^4} = E B^{-1}-2JL/R^3 \approx E B^{-1} = \frac{E}{1-\frac{2M}{R}} \approx E (1+\frac{2M}{R})##

##\displaystyle \dot{\phi} = \frac{R^2 B L+2JER}{R^4+4J^2} \approx \frac{R^2 B L+2JER}{R^4} = \frac{BL}{R^2}+\frac{2JE}{R^3} \approx \frac{BL}{R^2} =\frac{L}{R^2} (1-\frac{2M}{R}) \approx \frac{L}{R^2} ##

but I don't get the correct effective potential. Rather, doing ##\frac{dV}{dr} (r=R)=0## I don't get the expressions for E and L. Any ideas?
 
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One approach to solving this problem is to first consider the equations of motion for a test particle in the equatorial plane. These can be written as:

##\ddot{r} = -\frac{1}{2} \frac{d}{dr} (g_{tt} + 2g_{t\phi} \dot{\phi} + g_{\phi\phi} \dot{\phi}^2)##
##\ddot{\phi} = -\frac{1}{2} \frac{d}{dr} (g_{t\phi} + g_{\phi\phi} \dot{r}^2)##

Substituting in the Schwarzschild metric and setting ##\theta = \pi/2##, we get:

##\ddot{r} = -\frac{M}{r^2} + \frac{J^2}{r^3}##
##\ddot{\phi} = \frac{2J}{r^3}##

Now, for a test particle in a stable circular orbit at radius ##r = R##, we know that ##\ddot{r} = 0## and ##\dot{\phi} = \omega##, where ##\omega## is the orbital frequency. Plugging this in and solving for ##E## and ##L##, we get:

##E = \sqrt{1 - \frac{2M}{R}}##
##L = \frac{J}{\sqrt{1 - \frac{2M}{R}}}##

We can also use the equations of motion to find the effective potential, which is given by:

##V_{eff} = \frac{1}{2} \left( \frac{L^2}{r^2} + \frac{J^2}{r^4} \right) - \frac{M}{r}##

Plugging in our expressions for ##E## and ##L## and expanding to first order in ##M/R## and ##(J/R)^2##, we get:

##V_{eff} \approx \frac{1}{2} \left( 1 - \frac{2M}{R} \right) - \frac{M}{R} = \frac{1}{2} - \frac{3M}{2R}##

Setting ##dV_{eff}/dr = 0## and solving
 

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