SSC/Stability/n1PolytropeLAWE/Pt4: Difference between revisions

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     <ul>
     <ul>
       <li>[[SSC/Structure/BiiPolytropes/FreeEnergy51|One Discussion]]</li>
       <li>[[SSC/Structure/BiiPolytropes/FreeEnergy51|One Discussion]]</li>
       <li>[[SSC/Structure/BiPolytropes/Analytic51/Pt4|Another Discussion]]</li>
       <li>[[SSC/Structure/BiPolytropes/Analytic51/Pt4|Another Discussion]] <font color="red"> <==  Very Useful Analytic Integrals</font></li>
     </ul>
     </ul>
   </li>
   </li>

Revision as of 19:37, 10 August 2025

Radial Oscillations of n = 1 Polytropic Spheres (Pt 4)


Part I:   Search for Analytic Solutions
 

Part II:  New Ideas
 

Part III:  What About Bipolytropes?
 

Part IV:  Most General Structural Solution
 

Preamble Regarding Chatterji

As far as we have been able to ascertain, the first technical examination of radial oscillation modes in n=1 polytropes was performed — using numerical techniques — in 1951 by L. D. Chatterji; at the time, he was in the Mathematics Department of Allahabad University. His two papers on this topic were published in, what is now referred to as, the Proceedings of the Indian National Science Academy (PINSA). The citations that immediately follow this opening paragraph provide inks to both of these papers by Chatterji, but the links may be insecure. Apparently Springer is archiving recent PINSA volumes, but their holdings do not date back as early as 1951.

A detailed review of Chatterji51 is provided in an accompanying discussion.

Equilibrium Structure

When n=1, the relevant Lane-Emden equation is,

1ξ2ddξ(ξ2dΘHdξ)=ΘH ,

and we find that the solution is, quite generally,

θ

=

A[sinξξ]B[cosξξ]=1ξ{AsinξBcosξ}

in which case,

dθdξ

=

ddξ{A[sinξξ]B[cosξξ]}

 

=

A[sinξξ2+cosξξ]+B[cosξξ2+sinξξ]

 

=

1ξ2[Asinξ+Bcosξ]+1ξ[Acosξ+Bsinξ],

and,

Q(ξ)dlnθdlnξ

=

ξθ{1ξ2[Asinξ+Bcosξ]+1ξ[Acosξ+Bsinξ]}

 

=

1ξθ{[AsinξBcosξ]+ξ[AcosξBsinξ]}

 

=

{1ξ[Acosξ+BsinξAsinξBcosξ]}.

If we set βtan1(B/A), we can rewrite the expression for θ as,

θ

=

Aξ{sinξBAcosξ}

 

=

Aξ{sinξtanβcosξ}

 

=

Aξcosβ{sinξcosβcosξsinβ}

 

=

Acosβsin(ξβ)ξ,

Beech88, §3, p. 221, Eq. (6)
EFC98, §2, p. 831, Eq. (2)

and the expression for Q as,

Q(ξ)

=

{1ξ[cosξcosβ+sinξsinβsinξcosβcosξsinβ]}

 

=

{1ξ[cos(ξβ)sin(ξβ)]}

 

=

[1ξcot(ξβ)].

SUMMARY of EQUILIBRIUM STRUCTURE
and switching notation from θ(ξ) to ϕ(η)

When n=1, the relevant Lane-Emden equation is,

1η2ddη(η2dϕdη)=ϕ .

Its solution, quite generally, is

ϕ

=

A[sinηη]B[cosηη],

where A and B are scalar constants, in which case,

Q(η)dlnϕdlnη

=

{1η[Acosη+BsinηAsinηBcosη]}.


Alternatively, drawing from Eq. (6) of Beech88, this solution can be written in the form,

ϕ

=

αBeechsin(ηβBeech)η,

in which case,

Q(η)

=

[1ηcot(ηβBeech)],

where, in terms of the coefficients A and B,

βBeech

tan1(B/A)

      and      

αBeech

AcosβBeech=A[1+(B/A)2]1/2.

Establish Relevant (n=1) LAWE

From a related discussion — or a broader overview of Instability Onset — we find the

Polytropic LAWE (linear adiabatic wave equation)

0=d2xdξ2+[4(n+1)Q]1ξdxdξ+(n+1)[(σc26γg)ξ2θαQ]xξ2

where:    Q(ξ)dlnθdlnξ,    σc23ω22πGρc,     and,     α(34γg)

Furthermore — see, for example, here,

Exact Solution to the Polytropic LAWE

xP3(n1)2n[1+(n3n1)(1ξθn)dθdξ],

in which case for n=1,

xP=3(1ξθ)dθdξ=3(1ξ2)dlnθdlnξ=3ξ2Q.


Isolated Sphere

For an isolated n = 1 (γg=2,α=1) polytrope, we know that,

θ

=

sinξξ

    Q(ξ)dlnθdlnξ

=

[1ξcotξ].

Hence, the relevant LAWE is,

0

=

d2xdξ2+[42(1ξcotξ)]1ξdxdξ+2[(σc212)ξ3sinξ(1ξcotξ)]xξ2

LAWE for n = 1 Polytrope

0

=

d2xdξ2+2ξ[1+ξcotξ]dxdξ+12[(σc23)ξsinξ4ξ2(1ξcotξ)]x

Surface boundary condition:

dlnxdlnξ|surf

=

(3nn+1)+nσc26(n+1)[ξθ]surf

dlnxdlnξ|surf

=

1+σc212[ξ3(ξcosξsinξ)]ξ=π=1π2σc212

Spherical Shell

In the context of a spherically symmetric n = 1 (γg=2,α=1) shell (envelope) outside of a spherically symmetric bipolytropic core, we should adopt the more general Lane-Emden structural solution,

θ

=

A[sinξξ]B[cosξξ]

    Q(ξ)dlnθdlnξ

=

[1ξcot(ξβ)]=ξ2xP3.

Reminder: the expression for xP is,

xP=3ξ2[1ξcot(ξβ)].

Playing around a bit, we find that,

ξ23xP = 1ξcos(ξβ)sin(ξβ)
  = 1ξ[cos(ξβ)sin(ξβ)](ξβ)(ξβ)
  = 1ξ[cos(ξβ)(ξβ)][(ξβ)sin(ξβ)]

As a result, the governing LAWE becomes,

0 = d2xPdξ2+[42Q]1ξdxPdξ+2[(σc212)0ξ2θQ]xPξ2
  = d2xPdξ2+4ξdxPdξ[2Q]1ξdxPdξ[2Q]xPξ2
  = d2xPdξ2+4ξdxPdξ2Q{1ξdxPdξ+xPξ2}
  = d2xPdξ2+4ξdxPdξ2ξ2xP3{1ξdxPdξ+xPξ2}
  = d2xPdξ2+[4ξ2ξxP3]dxPdξ2xP23.

Let's plug in the expression for xP, namely, xP=3[1ξcot(ξβ)]/ξ2. We have, first of all,

xp2 = 32ξ4[1ξcot(ξβ)]2

 

= 32ξ4[12ξcot(ξβ)+ξ2cot2(ξβ)];

dxpdξ

= ddξ{3ξ2[1ξcot(ξβ)]}

 

= [1ξcot(ξβ)]ddξ{3ξ2}3ξddξ[cot(ξβ)]3ξ2[cot(ξβ)]

 

= 6ξ3[1ξcot(ξβ)]+3ξ[1+cot2(ξβ)]3ξ2[cot(ξβ)]

 

= 6ξ3+3ξ2[cot(ξβ)]+3ξ+3ξ[cot2(ξβ)].

Recognize that we have used the trigonometric relations,

ddξ[cot(u)]

= 1sin2(u)dudξ=[1+cot2(u)]dudξ.

And,

d2xpdξ2

= ddξ{6ξ3+3ξ+3ξ2[cot(ξβ)]+3ξ[cot2(ξβ)]}

 

= 18ξ43ξ26ξ3[cot(ξβ)]3ξ2[1+cot2(ξβ)]3ξ2[cot2(ξβ)]6ξ[cot(ξβ)][1+cot2(ξβ)]

 

= 18ξ46ξ26ξ3[cot(ξβ)]6ξ2cot2(ξβ)6ξ[cot(ξβ)]6ξcot3(ξβ).

Hence,

d2xPdξ2+[4ξ2ξxP3]dxPdξ2xP23

= {18ξ46ξ26ξ3[cot(ξβ)]6ξ2cot2(ξβ)6ξ[cot(ξβ)]6ξcot3(ξβ)}

 

  +[4ξ2ξxP3]{6ξ3+3ξ2[cot(ξβ)]+3ξ+3ξ[cot2(ξβ)]}

 

  {6ξ4[12ξcot(ξβ)+ξ2cot2(ξβ)]}

 

= 18ξ46ξ26ξ3[cot(ξβ)]6ξ[cot(ξβ)]6ξ2cot2(ξβ)6ξcot3(ξβ)

 

  +4ξ{6ξ3+3ξ2[cot(ξβ)]+3ξ+3ξ[cot2(ξβ)]}

 

  +[2ξxP3]{6ξ33ξ2[cot(ξβ)]3ξ3ξ[cot2(ξβ)]}

 

  +6ξ4[1+2ξcot(ξβ)ξ2cot2(ξβ)]

 

= 18ξ46ξ26ξ3[cot(ξβ)]6ξ[cot(ξβ)]6ξ2cot2(ξβ)6ξcot3(ξβ)

 

  24ξ4+12ξ3[cot(ξβ)]+12ξ2+12ξ2[cot2(ξβ)]

 

  +2ξ[1ξcot(ξβ)]{6ξ33ξ2[cot(ξβ)]3ξ3ξ[cot2(ξβ)]}

 

  +6ξ4[1+2ξcot(ξβ)ξ2cot2(ξβ)]

 

= 6ξ4+6ξ2+6ξ3[cot(ξβ)]6ξ[cot(ξβ)]+6ξ2cot2(ξβ)6ξcot3(ξβ)

 

  12ξ3cot(ξβ)+6ξcot(ξβ)+6ξ2[cot2(ξβ)]+6ξ[cot3(ξβ)]

 

  +12ξ46ξ3[cot(ξβ)]6ξ26ξ2[cot2(ξβ)]

 

  6ξ4+12ξ3cot(ξβ)6ξ2cot2(ξβ)

 

= 6ξ[cot(ξβ)]+6ξ2cot2(ξβ)6ξcot3(ξβ)

 

  +6ξcot(ξβ)+6ξ2[cot2(ξβ)]+6ξ[cot3(ξβ)]

 

  12ξ2[cot2(ξβ)]

 

= 0.

Debugging LaTeX layout:

 

  12ξ2[cot2(ξβ)]

 

  12ξ2[cot3(ξβ)]

 

 

+[cot1(ξβ)]+6ξ2[cot2(ξβ)m]+6ξ[cot3(ξβ)]

See Also

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