ParabolicDensity/GravPot

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Parabolic Density Distribution


Part I:   Gravitational Potential

 


Part II:   Spherical Structures

 


Part III:   Axisymmetric Equilibrium Structures

 


Part IV:   Triaxial Equilibrium Structures (Exploration)

 

Gravitational Potential

In an accompanying chapter titled, Properties of Homogeneous Ellipsoids (1), we have shown how analytic expressions may be derived for the gravitational potential inside of uniform-density ellipsoids. In that discussion, we largely followed the derivations of [EFE]. In the latter part of the nineteenth-century, 📚 N. M. Ferrers (1877, Quart. J. Pure Appl. Math., Vol. 14, pp. 1 - 22) showed that very similar analytic expressions can be derived for ellipsoids that have certain inhomogeneous mass distributions. Here we specifically discuss the case of configurations that exhibit concentric ellipsoidal iso-density surfaces of the form,

ρ

=

ρc[1(x2a12+y2a22+z2a32)],

that is, configurations with parabolic density distributions. Much of our presentation, here, is drawn from our separate, detailed description of what we will refer to as Ferrers potential.

Uniform-Density Reminders

We begin by reminding the reader that, for a uniform-density configuration, the "interior" potential will be given by the expression,

Φgrav(𝐱)

=

πGρc[IBTa12(A1x2+A2y2+A3z2)].

As we have shown in a separate presentation, if the three principal axes of the configuration are unequal in length and related to one another such that a1>a2>a3, the appropriate expressions for the four leading coefficients are,

A1

=

2a2a3a12[F(θ,k)E(θ,k)k2sin3θ];

A2

=

2a2a3a12[E(θ,k)(1k2)F(θ,k)(a3/a2)k2sinθk2(1k2)sin3θ];

A3

=

2a2a3a12[(a2/a3)sinθE(θ,k)(1k2)sin3θ];

IBT

=

2a2a3a12[F(θ,k)sinθ].

[EFE], Chapter 3, Eqs. (33), (34) & (35)

As can readily be demonstrated, this scalar potential satisfies the differential form of the

Poisson Equation

2Φ=4πGρ

As we have also demonstrated, if the longest axis, a1, and the intermediate axis, a2, of the ellipsoid are equal to one another, then an equatorial cross-section of the object presents a circle of radius a1 and the object is referred to as an oblate spheroid. For homogeneous oblate spheroids, evaluation of the integrals defining Ai and IBT gives,

A1

=

1e2[sin1ee(1e2)1/2](1e2)1/2;

A2

=

A1;

A3 =

2e2[(1e2)1/2sin1ee](1e2)1/2;

IBT =

2A1+A3(1e2)=2(1e2)1/2[sin1ee],

[EFE], Chapter 3, Eq. (36)
[T78], §4.5, Eqs. (48) & (49)

where the eccentricity,

e[1(a3a1)2]1/2.

Note the following, separately derived limits:

Table 1:  Limiting Values

 

e0

a3a10

sin1ee

1+e26+𝒪(e4)

π2(a3a1)+π4(a3a1)2𝒪(a33a13)

A1=A2

23[1e25𝒪(e4)]

π2(a3a1)2(a3a1)2+𝒪(a33a13)

A3

23[1+2e25+𝒪(e4)]

2π(a3a1)+4(a3a1)2𝒪(a33a13)

IBT

2

0

Hence, for a uniform-density sphere (e=0),

Φgrav(𝐱)

=

πGρc[IBTa12(A1x2+A2y2+A3z2)]

 

=

πGρc[2a1223(x2+y2+z2)]

 

=

2πGρca12[113(ra1)2]

 

=

3GM2a1[113(ra1)2].

J. B. Tatum (2021) Celestial Mechanics class notes (UVic), §5.8.9, p. 36, Eq. (5.8.23)

This matches the expression for the gravitational potential inside (and on the surface) of a uniform-density sphere, as we have derived in an accompanying chapter.

See Also

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