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aditya23456
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Is there any such relation as per general theory of relativity?
aditya23456 said:Is there any such relation as per general theory of relativity?
aditya23456 said:Is there any such relation as per general theory of relativity?
julian said:One answer is that if you are moving your mass is greater so the grav force increases, but...(thought experiment) say you have a speed boat at rest, the wieght (due to GRAVITY) equals the force due to water pressure. But what if the boat is moving at speed v with respect to the ocean? The area is reduced by [itex]\gamma[/itex] because of length conrtraction, plus the mass increases and hence the weight of the boat increases...the conclusion is that the boat will sink...
Are you sure about this ? After a proper acceleration the geodesic certainly does change but a body on a geodesic may have changing velocity.tom.stoer said:it's simple: when the velocity of the test particle changes, its geodesic changes as well
tom.stoer said:sorry for the confusion, the formulation is missleading; what I want to say is that test masses at one spacetime point P starting in one direction but with different initial velocities v, v', v'', ... will follow different geodesics C, C', C'', ...
In a sense, yes.aditya23456 said:Is there any such relation as per general theory of relativity?
D H said:One way to answer this question is to look at things from the perspective of a parameterized post-Newtonian (PPN) formalism. Here gravity is still a "force" but it isn't quite Newtonian gravity. In addition to good old F=GMm/r2, there are some first order perturbation terms that result from general relativity in such a formalism. These perturbative effects on Newtonian gravity involve velocity.
They're a bit more complex (well, more than a bit more complex) than that. See equation 8.1 in http://iau-comm4.jpl.nasa.gov/XSChap8.pdf , for example (this is what JPL uses), or see equation 10.12 in http://www.iers.org/nn_11216/SharedDocs/Publikationen/EN/IERS/Publications/tn/TechnNote36/tn36__151,templateId=raw,property=publicationFile.pdf/tn36_151.pdf .clamtrox said:Do you know if the corrections are in first order what you would expect by naive thinking, ie. F->F(1+v2/c2/2), or something different?
D H said:They're a bit more complex (well, more than a bit more complex) than that. See equation 8.1 in http://iau-comm4.jpl.nasa.gov/XSChap8.pdf , for example (this is what JPL uses), or see equation 10.12 in http://www.iers.org/nn_11216/SharedDocs/Publikationen/EN/IERS/Publications/tn/TechnNote36/tn36__151,templateId=raw,property=publicationFile.pdf/tn36_151.pdf .
That's off by a factor of three.clamtrox said:So basically yes, except it's hard to decide what the coefficient in place of 1/2 is because they are using vectors :) The equation in IERS document is pretty simple: first you have the correction from Schwarzschild metric, then two terms which look like v^2/c^2, and then corrections O(c^-4) which contain angular momentum and then it gets properly confusing, but we can drop those for now. The last term looks like some kind of angular momentum correction from the Sun, so let's drop that one too because we don't care about that... Finally, let's just be lazy and say we're on a circular orbit so [itex] \mathbf{r} \cdot \mathbf{\dot{r}} = 0 [/itex] and that it's general relativity so [itex] \gamma = 1 [/itex] and we're left with just
[itex] \Delta |\mathbf{a}| = \frac{GMv^2}{c^2 r^2} [/itex] which is actually twice as big as you'd expect. Is that about right?
clamtrox said:So basically yes, except it's hard to decide what the coefficient in place of 1/2 is because they are using vectors :) The equation in IERS document is pretty simple: first you have the correction from Schwarzschild metric, then two terms which look like v^2/c^2, and then corrections O(c^-4) which contain angular momentum and then it gets properly confusing, but we can drop those for now. The last term looks like some kind of angular momentum correction from the Sun, so let's drop that one too because we don't care about that... Finally, let's just be lazy and say we're on a circular orbit so [itex] \mathbf{r} \cdot \mathbf{\dot{r}} = 0 [/itex] and that it's general relativity so [itex] \gamma = 1 [/itex] and we're left with just
[itex] \Delta |\mathbf{a}| = \frac{GMv^2}{c^2 r^2} [/itex] which is actually twice as big as you'd expect. Is that about right?
What gives is that those other references such as my first one are not valid for a satellite in Earth orbit. That equation in the second article I referenced gives the perturbative effect Δa. It does not say how to compute the non-relativistic aspects of the acceleration; that's an exercise left to the reader.PAllen said:One thing I don't understand is that versions of these approximate GR equations of motion I've seen before (like the first of DH references), have acceleration in a term on the right . This version does not. What gives?
julian said:Yeah but when the strengh of grav field, speed and masses are so small you got to conceed that such considerations are valid.
D H said:What gives is that those other references such as my first one are not valid for a satellite in Earth orbit. That equation in the second article I referenced gives the perturbative effect Δa. It does not say how to compute the non-relativistic aspects of the acceleration; that's an exercise left to the reader.
You can't pretend that the only perturbations to spherical gravity are due to other bodies and general relativity. For an artificial satellite, atmospheric drag is huge for vehicles in low Earth orbit, and the non-spherical nature of Earth's gravity field dominates over relativistic effects out to order 20 or so even out to geosynchronous orbit. Even solar radiation pressure swamps relativistic effects.
The same goes for orbits about the Earth's moon. Low lunar orbits are very bizarre.
pervect said:Unfortunately, approximations that require that the speed be small (for instance the PPN formalism, i.e. Paramterized Post Newtonian approximations) can't really address the issue of how speed affects gravity, because the speed has already been assumed to be small.
The biggest pitfall to watch out for in trying to treat gravity as a "force" is how it behaves in different reference frames. I'm not aware of anything that plays the role of "force" in full GR that transforms like a tensor (much less like a 4-vector, which is what one expects a force to transform like).
The closest candidate I'm aware of are the Christoffel symbols - which are not tensors, and have the wrong rank as well.
This argument may sound technical, and it is - but not transforming properly ultimately leads to a lot of confusion. It breaks the usual way in which physics summarizes all the different things that different observers might measure into a single, unified, observer-independent framework.
In fact, I think that trying to understand how gravity transforms between different frames , how it appears to different observers, may be the root of the OP's question.
PAllen said:Maybe I'm blind, but I don't see any O(c^-4) corrections. I definitely agree we can dispense with the J terms for simplicity - consider the hypothetical non-spinning earth. I also agree it makes sense to pretend the sun doesn't exist, for simplicity, so that leaves only the first line.
Then, using your circular orbit suggestion, I get something different:
4(GM)^2/(c^2 r^3) - (GM/r^2) (v^2/c^2)
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One thing I don't understand is that versions of these approximate GR equations of motion I've seen before (like the first of DH references), have acceleration in a term on the right . This version does not. What gives?
[Edit: I see DH posted first. Fortunately, our comments are similar.]
I just got to know that my question was valid ie answer to my question is yes and at the same time explaining this effect needs mathematics which is beyond my undergraduate level but surely I ll try to understand what u all meant
See my answer here:http://physics.stackexchange.com/qu...al-gravitation-is-really-a-square/22025#22025clamtrox said:Do you know if the corrections are in first order what you would expect by naive thinking, ie. F->F(1+v2/c2/2), or something different?
jimgraber said:See my answer here:
http://physics.stackexchange.com/qu...al-gravitation-is-really-a-square/22025#22025
The leading order PPN correction involves a v^2/c^2, but also a 3 and a 1/r^2. So its not quite the same as you would naively expect.
Naty1 said:Do you have an example relating to your question?
For example, as the Earth revolves around the sun is the 'force' on each different? Are the 'speeds' different? Would the force on each be different than the first case if the Earth were plunging towards the sun? How about a pair of photons traveling along side by side in the same direction compared with traveling in opposite directions?
A bunch of the 'latter' answers here are pretty far afield from your question... as experts are discussing stuff with each other.