Template:LSU CT99CommonTheme2

From JETohlineWiki
Revision as of 18:45, 21 June 2024 by Joel2 (talk | contribs) (Created page with "Suppose we rewrite (Version 1 of) the above-highlighted Key integral expression such that the (primed) coordinate location of each mass element is mapped from cylindrical coordinates <math>~(\varpi^', z^')</math> to a toroidal-coordinate system <math>~(\eta^',\theta^')</math> whose ''anchor ring'' cuts through the meridional plane at the cylindrical-coordinate location, <math>~(\varpi_a,z_a)</math>. This desired mapping is handled via the pair of relations,...")
(diff) ← Older revision | Latest revision (diff) | Newer revision → (diff)
Jump to navigation Jump to search

Suppose we rewrite (Version 1 of) the above-highlighted Key integral expression such that the (primed) coordinate location of each mass element is mapped from cylindrical coordinates (ϖ',z') to a toroidal-coordinate system (η',θ') whose anchor ring cuts through the meridional plane at the cylindrical-coordinate location, (ϖa,za). This desired mapping is handled via the pair of relations,

ϖ'=ϖasinh⁡η'(cosh⁡η'−cos⁡θ'),

      and      

(z'−za)=ϖasin⁡θ'(cosh⁡η'−cos⁡θ'),

and the corresponding expression for each differential mass element is,

δM(η',θ')=[2πϖa3sinh⁡η'(cosh⁡η'−cos⁡θ')3]ρ(η',θ')dη'dθ'.

This gives, what we will refer to as the,

Gravitational Potential of an Axisymmetric Mass Distribution (Version 2)

Φ(ϖ,z)|axisym

=

−Gπ∬config[μϖ1/2][ϖasinh⁡η'(cosh⁡η'−cos⁡θ')]−1/2K(μ)[2πϖa3sinh⁡η'(cosh⁡η'−cos⁡θ')3]ρ(η',θ')dη'dθ'

 

=

−2G(ϖa5ϖ)1/2∬config[sinh⁡η'(cosh⁡η'−cos⁡θ')5]1/2μK(μ)ρ(η',θ')dη'dθ',

where the square of the argument of the elliptic integral is,

μ2

=

4ϖϖasinh⁡η'(cosh⁡η'−cos⁡θ'){[ϖ+ϖasinh⁡η'(cosh⁡η'−cos⁡θ')]2+[z−za−ϖasin⁡θ'(cosh⁡η'−cos⁡θ')]2}−1.