Astron. Astrophys. 356, 218-233 (2000)
Appendix A
The aim of this appendix is to explain in a detailed way how to
obtain the boundary condition .
A.1. Set of equations
The full set of linearized ideal MHD equations in the case of
adiabatic oscillations is
-
- the equation of motion
![[EQUATION]](img374.gif)
-
- the conservation of mass
![[EQUATION]](img375.gif)
-
- the adiabatic condition
![[EQUATION]](img376.gif)
-
- the equation of induction
![[EQUATION]](img377.gif)
where the quantities ,
,
denote the Eulerian perturbations of the pressure, density and the
magnetic field, and ,
denote the Lagrangian perturbation
of the pressure and the density. The temporal dependence is assumed to
be . The displacement
and the Lagrangian perturbation of
pressure are given by Eq. 3 and Eq. 4. As we consider high
frequencies, we adopt the Cowling approximation, i.e. we neglected the
perturbation of the gravitational potential,
.
In order to simplify this system of equations, we have made several
assumptions. First, we assumed large radial wave numbers,
therefore,
![[EQUATION]](img385.gif)
where X is any perturbed quantity. More, we suppose that
horizontal wave numbers are small compared with radial wave numbers,
ie
![[EQUATION]](img386.gif)
We also assumed . The result for
the Lorentz force with these approximations is given by Eq. 6-8.
After simplifications thanks to the previous assumptions and a little
algebra, we get the following system
![[EQUATION]](img388.gif)
A.7 is the equation of continuity, A.8 the equation of motion on
, A.10 the equation of motion on
, A.12 the equation of motion on
. A.9, A.11 have been introduced to
get a system of differential equations of the first order.
The following variables have been introduced
![[EQUATION]](img391.gif)
and
![[EQUATION]](img392.gif)
with defined by Eq. 1.
V and are defined by
![[EQUATION]](img394.gif)
We also introduced the dimensionless frequency
by
![[EQUATION]](img396.gif)
with the range of frequencies we consider in this paper [1200,2300]
, it corresponds to a range of [10,19]
for .
We see that the system Eq. A.7-A.12 is singular at the pole
and the equator. These two limit cases needs a special treatment (see
Appendix B)
The upper and lower boundaries of the magnetic layer depend, as
expected, on the value of the photospheric magnetic field
. For the top of this layer, we
required that tends to vacuum field
( ) as
tends to zero. Therefore, we can
put the right hand side of Eq. A.10 and Eq. A.12 equal to
zero. This requires us to extend the atmosphere sufficiently high to
have low density and then verify .
At the base of the magnetic layer we need two conditions. The first
one corresponds to a negligible magnetic pressure compared with the
gas pressure; for this we require .
The second condition concerns Alfvénic waves. We require that
their wavelengths are much shorter than the pressure scale height,
i.e. . We give in Table 1
several values of at the top and
the base of the magnetic layer.
![[TABLE]](img407.gif)
Table 1. Limits of the magnetic boundary layer for different values of the magnetic fields, and in each case, the value of the two parameters and describing the importance of the magnetic field.
The general solution vector of
this system can be written as a linear combination of six linearly
independent solutions. However, we assume that the star is an isolated
system, i.e. we reject inward propagating waves which could come from
infinity. Hence, this reduces our solutions to three inside the
magnetic layer
![[EQUATION]](img409.gif)
There are two steps in the numerical integration. The first one
consists of finding the three peculiar solutions
for each radial position x
in the magnetic layer. To do this, we start from the top of the layer
with analytical peculiar solutions which are found thanks to a local
analysis. We then integrate them numerically, with a method of
Runge-Kutta, through the magnetic layer to the base
( ). The next step of the numerical
integration is to find the coefficients of the linear combination
. This is done at the base of the
boundary layer adding another condition. Since at
one has
, we assumed a full decoupling
between p-modes and Alfvénic modes beneath the magnetic layer.
We add also the condition that there are only inwards propagative
Alfvénic waves under the magnetic layer (see also Roberts &
Soward 1983). Then the solution at the base of the magnetic layer has
the following form
![[EQUATION]](img413.gif)
The Alfvénic solutions
are obtained with a WKBJ method. The components of
at the fit only depend on the two
variables and
. (see below). Therefore, the unknown
quantities are and
which are found matching the
solutions Eq. A.18 and Eq. A.19. This leads to a linear
homogeneous system of equations which has non trivial solutions if the
secular determinant is zero. This condition gives the relation between
and
at
, that is to say the boundary
condition .
A.2. External boundary conditions
We adopted here a local analysis of the system assuming that the
coefficients of the system Eq. A.7-A.12 are constant (we assume
to be in an isothermal atmosphere). The solutions have the form
. This gives a relation of
dispersion
![[EQUATION]](img420.gif)
One gets three groups of solutions. As said before, we keep only
outward propagating or decreasing waves in the atmosphere. The
solution may be written as
![[EQUATION]](img421.gif)
The three remaining solutions correspond to three different waves
numbers of Eq. A.20.
The first one is
![[EQUATION]](img422.gif)
being the dimensionless
non-magnetic acoustic cut-off frequency and is given by
![[EQUATION]](img424.gif)
The corresponding vector solution can be written as followed
![[EQUATION]](img425.gif)
where we choose the normalization condition
. The second type of solution obeys
the condition
![[EQUATION]](img427.gif)
This gives a second vector (with
)
![[EQUATION]](img429.gif)
For the last vector corresponding to the wave number
![[EQUATION]](img430.gif)
one can choose with (with
)
![[EQUATION]](img433.gif)
Next, each component of the vector S is integrated by a
method of Runge-Kutta of the fourth order with adapted step size. The
result is the values ,
and
.
A.3. Inner boundary conditions
To obtain the expression for these coefficients, we require new
conditions at the base of the magnetic layer. In this part of the
star, the ratio is very small. This
means that the Alfvénic speed is negligible compared with the
sound speed. Since the two perturbations of B and p, say
the Alfvénic waves and pressure waves are propagating with very
different speeds, it appears a decoupling between the two.
Mathematically, this decoupling appears in the system Eq. A.7-
A.12 because of the small value of .
Then, a solution of the system Eq. A.7-A.12 can be written as
![[EQUATION]](img438.gif)
The subscript "p" refers to the p-mode solution, whereas the
subscript "A" corresponds to the Alfvénic solution.
Since, the effect of the magnetic field is very small below the
magnetic layer, we can again use a perturbative approach to find the
solutions.
A.3.1. p-modes solution
This corresponds to the zeroth-order of perturbation,
. Then, Eq. A.7-Eq. A.12
reduces to
![[EQUATION]](img440.gif)
![[EQUATION]](img441.gif)
where we neglected the terms due to
since they are small compared with
and
as we can see on Eq. A.30. This
system corresponds to the system of equations in the case of
non-magnetic and adiabatic radial oscillations (in the Cowling
approximation).
we obtain
![[EQUATION]](img443.gif)
Then, we can write the vector solution for p-modes as function of
and
.
![[EQUATION]](img444.gif)
A.3.2. Alfvénic modes
This corresponds to the first order of perturbations in
. We suppose for Alfvénic
waves that and also
. The system governing the
Alfvénic waves is
![[EQUATION]](img448.gif)
To solve this system we use a WKBJ approach with the form
![[EQUATION]](img449.gif)
k obeys the following relation of dispersion
![[EQUATION]](img450.gif)
with
![[EQUATION]](img451.gif)
We keep only solutions which propagate inwards. One has, then, two
kinds of solutions
-
solution with
![[EQUATION]](img453.gif)
-
solution with
![[EQUATION]](img455.gif)
Then, at the base of the magnetic layer
the inner boundary condition write
as
![[EQUATION]](img456.gif)
can be written as the following system of algebraic linear
equations
![[EQUATION]](img457.gif)
The solutions with the subscripts 1, 2, 3 are the values at
after integration in the boundary
layer, and the solutions with the subscript "A" are given by
Eq. A.42 and A.43. Requiring that the determinant of the matrix
in Eq. A.45 is zero, one obtains the function
.
Appendix B
The results presented in the previous section are not valid at the
pole ( ) and the equator
( ) because of the singular behaviour
of the equations. For these two points we need to find two systems of
equations.
B.1. The pole
At the pole the Lorentz force vanishes. Therefore, the system of
equations reduces to the second order Eq. A.30-A.32 (i.e. the
system for radial p-modes in the non-magnetic and adiabatic case)
B.2. The equator
At the equator the Lorentz Eq. 6-8 gets a simpler
expression
![[EQUATION]](img460.gif)
![[EQUATION]](img461.gif)
![[EQUATION]](img462.gif)
It can be shown that the system at the equator reduces to the
second order
![[EQUATION]](img463.gif)
with
![[EQUATION]](img464.gif)
![[EQUATION]](img465.gif)
Appendix C
The formula Eq. 33 provides a good test for numerical
calculations. Once the numerical solution is found the eigen vectors
are injected in the following formulas Eq. C.1-C.2 which leads to
another evaluation of the frequencies. We neglect the terms
corresponding to B since the eigen frequencies corresponds to
the oscillations below , i.e. where
the dynamical effect of B is negligible compared with the
effect of gas pressure.
We give hereafter the formulas for
and
obtained by taking the real and the
imaginary part of Eq. 33.
![[EQUATION]](img467.gif)
![[EQUATION]](img468.gif)
with
![[EQUATION]](img469.gif)
The relative differences between the numerical solutions of
and
with the frequencies calculated with
Eq. C.1 and Eq. C.2 are given in Fig. C.1. We see that
the consistency of the calculation are better than
for the real part and better than
0.01 for the imaginary part, for the mode
and
.
![[FIGURE]](img479.gif) |
Fig. C1. Relative differences between the numerical solution for the real frequency (left) and the imaginary frequency (right) with the frequency calculated with Eq. C.1 and Eq. C.2; for the mode , (full) and , (dashed) in Fig. 6.
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© European Southern Observatory (ESO) 2000
Online publication: March 28, 2000
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