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I don’t understand why this effect would not be…
I don’t understand why this effect would not be…
direct.mit.edu/books/book/4...
direct.mit.edu/books/book/4...
autonomousfx.com/fx-galleries...
autonomousfx.com/fx-galleries...
In the radial direction, the curvature is negative and twice as much (so that all three curvatures sum to zero, which is always true in a vacuum).
In the radial direction, the curvature is negative and twice as much (so that all three curvatures sum to zero, which is always true in a vacuum).
For other bodies and orbits, just scale the circumference with the orbital period.
For other bodies and orbits, just scale the circumference with the orbital period.
www.gregegan.net/SCIENCE/Bore...
Circular orbits are trickier. I don’t think you can embed a large enough submanifold in any three-dimensional space.
www.gregegan.net/SCIENCE/Bore...
Circular orbits are trickier. I don’t think you can embed a large enough submanifold in any three-dimensional space.
K A ≈ (1.707 × 10^{-23}) × (1.76 × 10^{13})
≈ 3 × 10^{-10} radians
That would not be easy to measure directly!
K A ≈ (1.707 × 10^{-23}) × (1.76 × 10^{13})
≈ 3 × 10^{-10} radians
That would not be easy to measure directly!
K = 1/R^2
= GM/(c^2 r^3)
≈ 1.707 × 10^{-23}
The sum of the angles of a triangle with area A in a space with curvature K is about π + K A, so if space at a fixed moment in time has a similar curvature to the spacetime curvature we’ve found …
K = 1/R^2
= GM/(c^2 r^3)
≈ 1.707 × 10^{-23}
The sum of the angles of a triangle with area A in a space with curvature K is about π + K A, so if space at a fixed moment in time has a similar curvature to the spacetime curvature we’ve found …
T = 5096 sec
and the radius of curvature of spacetime is:
R = 2.4 × 10^{11} metres
T = 5096 sec
and the radius of curvature of spacetime is:
R = 2.4 × 10^{11} metres
P = c T
and then the radius of curvature of spacetime is:
R = P / (2π) = c √[r^3/(GM)]
P = c T
and then the radius of curvature of spacetime is:
R = P / (2π) = c √[r^3/(GM)]
For an orbit with radius r around a mass M, the period of the orbit is:
T = 2π √[r^3/(GM)]
where G is the gravitational constant.
For an orbit with radius r around a mass M, the period of the orbit is:
T = 2π √[r^3/(GM)]
where G is the gravitational constant.