2014
DOI: 10.48550/arxiv.1410.6265
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Marginally stable circular orbit of a test body in spherically symmetric and static spacetimes

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“…where e ∈ (0, 1) is the orbital eccentricity. Now consider the HPM solution of the equation (24). For this purpose, we suppose the following homotopy…”
Section: Computation Of Precession Angle In Bbmb Spacetime Using Hpmmentioning
confidence: 99%
“…where e ∈ (0, 1) is the orbital eccentricity. Now consider the HPM solution of the equation (24). For this purpose, we suppose the following homotopy…”
Section: Computation Of Precession Angle In Bbmb Spacetime Using Hpmmentioning
confidence: 99%