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Geodesics of the Kerr metric

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<strong>the</strong>n<br />

The equation<br />

)<br />

2<br />

(r − Ma2 ω 2 + 4Ma ω − 2M =0. (4.85)<br />

r 2 r 2 r 2<br />

(r 3 − Ma 2 )ω 2 +2Maω − M =0 (4.86)<br />

has discriminant<br />

M 2 a 2 + M(r 3 − Ma 2 )=Mr 3 (4.87)<br />

and solutions<br />

ω ± = −Ma ± √ Mr 3<br />

= ± √ M r3/2 ∓ a √ M<br />

r 3 − Ma 2<br />

r 3 − Ma 2<br />

= ± √ r 3/2 ∓ a √ M<br />

M<br />

(r 3/2 + a √ M)(r 3/2 − a √ M)<br />

√<br />

M<br />

= ±<br />

r 3/2 ± a √ M . (4.88)<br />

This is <strong>the</strong> relation between angular velocity and radius <strong>of</strong> circular<br />

orbits, and reduces, in Schwarzschild limit a =0,to<br />

which is Kepler’s 3 rd law.<br />

ω ± = ±√<br />

M<br />

r 3 , (4.89)<br />

4.2 General geodesic motion: <strong>the</strong> Carter constant<br />

To study generic geodesics in <strong>Kerr</strong> spacetime, we need to apply<br />

<strong>the</strong> Hamilton-Jacobi approach, whichallowstoidentifyafur<strong>the</strong>r<br />

constant <strong>of</strong> motion (not related to anyisometry<strong>of</strong><strong>the</strong><strong>metric</strong>).<br />

To apply <strong>the</strong> Hamilton-Jacobi approach, we first have to express<br />

our system with an Hamiltonian description. Given <strong>the</strong> Lagrangian<br />

<strong>of</strong> <strong>the</strong> system<br />

L(x µ , ẋ µ )= 1 2 g µνẋ µ ẋ ν (4.90)<br />

84

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