Generalized Tetrad Formalism for Rotating Spacetimes and the Equatorial Plane

  • Context: Undergrad 
  • Thread starter Thread starter Vrbic
  • Start date Start date
  • Tags Tags
    Rotating Spacetime
Click For Summary

Discussion Overview

The discussion revolves around the tetrad formalism used to describe phenomena near Kerr black holes, particularly focusing on the Local Non-Rotating Frame (LNRF) and its application in the equatorial plane (EP) versus other latitudes. Participants explore the implications of frame dragging and the behavior of test particles in different orbital configurations.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested

Main Points Raised

  • One participant questions the form of the LNRF tetrad outside the equatorial plane and whether additional terms arise in the tetrad expressions.
  • Another participant confirms the use of Boyer-Lindquist coordinates and emphasizes that the tetrad's form in the equatorial plane is contingent on this choice of coordinates.
  • A participant suggests that the inability of test particles to orbit in a plane parallel to the EP indicates a force acting in the latitude direction, potentially leading to an extra term in the tetrad.
  • There is a discussion about the nature of orbits in Schwarzschild spacetime and how they relate to frame dragging when transitioning to a rotating black hole scenario.
  • Participants express that the tetrad should maintain the same form across different latitudes, although the relative values of its components may vary with latitude and radius.
  • Clarification is provided that while the same functions derived from the metric apply, the assumption of eliminating theta dependence in the equatorial plane does not yield the most general forms.

Areas of Agreement / Disagreement

Participants generally agree on the form of the tetrad being consistent across latitudes, but there is no consensus on the implications of frame dragging and the specific behavior of test particles in non-equatorial orbits. The discussion remains unresolved regarding the exact nature of the tetrad outside the equatorial plane.

Contextual Notes

Limitations include the dependence on specific coordinate choices and the assumptions made regarding the behavior of test particles in various gravitational fields. The discussion highlights the complexity of the relationships between different variables in the tetrad formalism.

Vrbic
Messages
400
Reaction score
18
I'm interested in tetrad formalism for describing phenomenons near Kerr black hole. I've read some papers and I have a question about Localy Non-Rotating Frame (LNRF). In all papers is mentioned that most of astrophysically important cases are in equatorial plane (EP) and deals with EP only. Such tetrade looks:
##\omega^{(t)}{\mu}=(A,0,0,0) ##
##\omega^{(r)}{\mu}=(0,B,0,0) ##
##\omega^{(\theta)}{\mu}=(0,0,C,0) ##
##\omega^{(\phi)}{\mu}=(-\Omega_{LNRF} D,0,0,D) ##, where ##A,B,C,D, \Omega_{LNRF}##
we can find out from definition of tetrad and metric.
But what about out of EP? Is LNRF tetrad still in same form? Or there arise some extra expressions? Or how can I prove it that it is same on all ##\theta##?
 
Physics news on Phys.org
Vrbic said:
what about out of EP? Is LNRF tetrad still in same form? Or there arise some extra expressions?

First, I assume you are using Boyer-Lindquist coordinates, since in other coordinates the tetrad in the equatorial plane would not have the form you give.

Second, where does the extra term in the fourth tetrad (the ##t## component) come from? Answering that should help to answer your questions about the form of the tetrad out of the equatorial plane?
 
PeterDonis said:
First, I assume you are using Boyer-Lindquist coordinates, since in other coordinates the tetrad in the equatorial plane would not have the form you give.
Definitely, Boyer - Lindquist coordinates.
 
PeterDonis said:
Second, where does the extra term in the fourth tetrad (the tt component) come from? Answering that should help to answer your questions about the form of the tetrad out of the equatorial plane?
I was thinking about situation out of EP. And I know other thing, for example test particle can't orbit in plane parallel to EP. For me it says, there is force which acts on it in latitude direction. So it seems to me similar as in EP with draging in direction of rotation. So if any I would expect extra term ##\omega^{(\theta)}_t##.
 
Vrbic said:
test particle can't orbit in plane parallel to EP.

Yes, that's correct.

Vrbic said:
For me it says, there is force which acts on it in latitude direction. So it seems to me similar as in EP with draging in direction of rotation.

Why? A test particle can't orbit in a plane parallel to the equatorial plane because such an orbit would not be centered on the hole. That would be just as true in Schwarzschild spacetime, where there is no frame dragging.
 
PeterDonis said:
Why? A test particle can't orbit in a plane parallel to the equatorial plane because such an orbit would not be centered on the hole. That would be just as true in Schwarzschild spacetime, where there is no frame dragging.
Yes, I see. Now I have new question: If I let the test particle to orbits in Schwarzschild spacetime out of my chosen equatorial plane (almost circle orbit - rosette shape -I don't know if it is good name) and then let the hole rotate (such that my equatorial plane will be real equatorial plane of rotating hole). The change of shape of orbit will be affected only by frame dragging or is it more complex?

So from what you said, the tetrad should be same for all ##\theta##. Do you agree?
 
Vrbic said:
If I let the test particle to orbits in Schwarzschild spacetime out of my chosen equatorial plane (almost circle orbit - rosette shape -I don't know if it is good name)

I don't understand what kind of orbit you are referring to. There are no orbits that are not centered on the hole. Are you just describing a non-circular orbit, which because of perihelion precession will not be a closed ellipse (as it would be in Newtonian gravity)?

Vrbic said:
then let the hole rotate (such that my equatorial plane will be real equatorial plane of rotating hole). The change of shape of orbit will be affected only by frame dragging or is it more complex?

AFAIK the only effect that comes into play when the hole is rotating vs. not rotating is frame dragging. The reason I asked about where the extra term in the equatorial plane came from was to focus on how frame dragging is reflected in the metric in your chosen coordinates, and in particular whether there is any difference in how it is reflected out of the equatorial plane vs. in the equatorial plane.
 
PeterDonis said:
I don't understand what kind of orbit you are referring to. There are no orbits that are not centered on the hole. Are you just describing a non-circular orbit, which because of perihelion precession will not be a closed ellipse (as it would be in Newtonian gravity)?
Yes, it is exactly what I've meant.
 
PeterDonis said:
AFAIK the only effect that comes into play when the hole is rotating vs. not rotating is frame dragging. The reason I asked about where the extra term in the equatorial plane came from was to focus on how frame dragging is reflected in the metric in your chosen coordinates, and in particular whether there is any difference in how it is reflected out of the equatorial plane vs. in the equatorial plane.
Oh, ok. So may I say because LNRF tetrad coming from kerr metric in Boyer - Lindquist coordinate which are same for all planes or there is no change in equatorial plane, LNRF tetrad has to have same shape for all latitude. Do you agree?
 
  • #10
Vrbic said:
LNRF tetrad has to have same shape for all latitude.

Meaning the same components are nonzero? I believe so, yes. But the relative values of those components vary with latitude (and also with radius).
 
  • Like
Likes   Reactions: Vrbic
  • #11
PeterDonis said:
Meaning the same components are nonzero? I believe so, yes. But the relative values of those components vary with latitude (and also with radius).
Definitely, I mean that there are still same functions (coming from metric).
So thank you very much for advices.
 
  • #12
Vrbic said:
I mean that there are still same functions (coming from metric).

As long as by "the same functions" you mean the most general ones derived from the metric, including the ##\theta## dependence as well as the ##r## dependence, yes, this is true. When restricting attention to the equatorial plane, people often eliminate the ##\theta## dependence by assuming ##\sin \theta = 1##. But the functions you get when you do that are not the most general ones.
 
  • Like
Likes   Reactions: Vrbic

Similar threads

  • · Replies 17 ·
Replies
17
Views
2K
  • · Replies 5 ·
Replies
5
Views
2K
  • · Replies 4 ·
Replies
4
Views
2K
  • · Replies 30 ·
2
Replies
30
Views
2K
  • · Replies 31 ·
2
Replies
31
Views
4K
  • · Replies 6 ·
Replies
6
Views
2K
  • · Replies 18 ·
Replies
18
Views
5K
  • · Replies 62 ·
3
Replies
62
Views
7K
  • · Replies 11 ·
Replies
11
Views
2K
  • · Replies 15 ·
Replies
15
Views
2K