A&A 366, 157-165 (2001)
DOI: 10.1051/0004-6361:20000217

What mimics the reflection effect in symbiotic binaries?[*]

A. Skopal

Astronomical Institute, Slovak Academy of Sciences, 05960 Tatranská Lomnica, Slovakia

Received 17 February 2000 / Accepted 19 October 2000

Abstract
We discuss the origin of a periodic wave-like variation as a function of the orbital phase observed in the light curves (LC) of symbiotic stars. It is shown that this type of variability cannot be ascribed to a reflection effect. For example, the observed amplitudes of the LCs are far larger than those calculated within a model of the reflection effect. Here, the nature of the orbitally related changes in the optical continuum is outlined within an ionization model of symbiotic binaries.

Key words: stars: binaries: symbiotic


1 Introduction

Symbiotic stars are interacting binaries consisting of a cool giant and a hot compact star. Typical orbital periods run between 1-3 years. The giant component losses mass, part of which is accreted by its companion. The hot star ionizes a portion of the giant's wind, giving rise to nebular emission. As a result the spectrum of symbiotic stars consists of basically three components of radiation - two stellar and one nebular. Such composition of the spectrum was demonstrated well for ZAnd, BFCyg and AGDra (Nussbaumer & Vogel 1989; Fernandéz-Castro et al. 1990; Greiner et al. 1997). In many cases the nebular radiation dominates the optical.

A very significant feature of LCs of many symbiotic stars is a periodic wave-like variation along the orbital motion (see Fig. 1). It displays a large amplitude (i.e. magnitude difference between the maximum and minimum of the light), $\Delta m \sim$1mag or more, which is a function of the wavelength - we always observe $\Delta U > \Delta B \mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hf...
...nterlineskip\halign{\hfil$\scriptscriptstyle .... The period is approximately equal to the orbital period, and a minimum occurs at/around the inferior conjunction of the cool component. These properties relate this type of variations to the orbital motion. Originally, Boyarchuck (1966) and Belyakina (1970) suggested a reflection effect as responsible for such variability in the AGPeg LC. In this model, the hot star irradiates and heats up the facing giant's hemisphere that causes variation in the star's brightness when viewing the binary at different orbital phases. This natural explanation was adopted by many authors (e.g. Kenyon 1986) and it is still popular (e.g. Munari 1989, 1992; Dobrzycka et al. 1993; Proga et al. 1996, 1998). On the other hand, some authors have never used the reflection effect and/or found it to be problematic to interpret their data. For example, Nussbaumer & Vogel (1987) suggested a new approach to symbiotic stars based on the interaction of the hot star radiation with the cool stellar wind. Formiggini & Leibowitz (1990) found that the reflection effect requires an extremely high bolometric luminosity of the hot component, to explain the light variation in AGDra, AXPer and AGPeg. Schmutz et al. (1994) did not find any irradiation effect in the red giant spectrum of SYMus, although its visual LC varies with an amplitude of 0.6mag. Recently Skopal (1996) demonstrated that the reflection effect is not a reliable interpretation of the wave-like variation in the optical continuum of V443Her.

Accordingly we show that the reflection effect cannot explain the orbitally related wave-like modulation of LCs of symbiotic binaries. To demonstrate this, we compare basic observational properties of this variation to those caused by the reflection effect (Sect. 3). In Sect. 4 we describe a simple ionization model, which could be responsible for such variation.

2 Observation

Figure 1 shows examples of the periodic wave-like variation in the UBV LCs for selected symbiotic stars. Table 1 summarizes its basic characteristics - the amplitude, $\Delta m$, and the profile through a parameter a (Sect. 3.2). Photometric UBV observations used in this paper has been extracted from the literature and are also referred in Table 1.

  \begin{figure}
\par\resizebox{\hsize}{!}{\includegraphics{ms9660f1ar.eps}\hspace...
...hics{ms9660f1kr.eps}\hspace*{5mm}
\includegraphics{ms9660f1lr.eps}}\end{figure} Figure 1: Examples of periodic wave-like variation in the LCs of selected symbiotic binaries. Symbols, $\bullet $, $\bigtriangleup $ and +, represent observations in the U, B and V band, respectively. Profiles of the LCs are characterized by the parameter $a \sim 0.5$ (left panels), 0.5 < a < 1 (mid) and $a \approx 1$ (right), see Sect. 3.2. In cases of a poor coverage of orbital cycles, the data were folded according to their photometric ephemerides. Sources of the data are given in Table 1


 

 
Table 1: Characteristics of the LC profile: the observed amplitude, $\Delta m$, and the shape, a, (Sect. 3.2)
Object $P_{\rm orb}$ $\beta^{\star}$ $\Delta U$ $\Delta B$ $\Delta V$ aU   aB   aV Obs. Note
AXPer 680 $0.02\pm0.008$ 0.8  0.6  0.5  0.6  0.7  0.8 1  
BFCyg 757 $0.4\pm0.12$ 1.1  0.9  0.8 0.5  0.6  0.6 2 ss
CICyg 855 $0.06\pm0.011$ 1.2  0.7  0.5 0.8  0.8  0.9 3 ss
EGAnd 482 $\le 0.002\pm0.001$ 0.6  0.3  0.2 1.0  1.0  1.0 4 sss
AGDra 550 $0.01\pm0.008$ 1.0  0.2  0.1 0.5  0.5  0.5 5  
V1329Cyg 958 0.18 -0.47 1.8  1.3  1.2 0.5  0.5  0.5 6  
He2-467 479 0.07 -0.2 2.2  0.6  0.3 0.6  0.6  1.0 7 s
ZAnd 759 $\mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hfil
$\displaystyle ... 1.5  1.0  0.7 0.5  0.5  0.6 8 ss
V443Her 594 $\sim$0.04 0.7  0.4  0.3 0.6  0.7  0.8 9  
AGPeg 813 $\sim$0.03 1.1  0.6  0.5 0.5  0.5  0.5 10  

$\star$ - see Appendix A for more detail.
Note: s - secondary minimum in V, ss - occasional presence of secondary minima in V, sss - secondary minima in U, B, V.
Obs.: 1 - Skopal (1998b), Skopal et al. (2000), 2 - Hric et al. (1994, 1996), Skopal et al. (1995, 1997), Skopal (1998b), 3 - Belyakina (1979, 1984, 1992), 4 - Skopal (1997), 5 - Hric et al. (1991, 1993, 1994), Kaler (1987), Kaler et al. (1987), Skopal et al. (1992, 1995), 6 - Arkhipova & Ikonnikova (1989), Chochol et al. (1999), 7 - Arkhipova & Noskova (1985, 1987, 1988), 8 - Belyakina (1986, 1992), 9 - Taranova & Yudin (1987), Belyakina (1992), Kolotilov et al. (1995), 10 - Belyakina (1965, 1970, 1992), Komárek (1990), Fernie (1985), Luthardt (1989), Tomov & Tomova (1998).

3 Properties of the wave-like variation

In this section we compare the observed parameters of the wave-like variation - its amplitude and profile - to those given by the reflection effect.

3.1 The amplitude of light curves

The largest amplitude, between $\sim$0.5 and $\sim$2.5mag, is observed in the U band (Fig. 1, Table 1). In the model of the reflection effect, it is given by the luminosity ratio of the illuminated to the non-illuminated giant's hemisphere. The upper limit ( $i=90^{\circ }$) of the magnitude difference between the two hemispheres, $\Delta m_{\rm max}$, can be expressed as

\begin{displaymath}\Delta m_{\rm max} = - 2.5\log (1 + 2 L_{\rm RE}/L_{\rm g}),
\end{displaymath} (1)

where $L_{\rm g}$ is the luminosity of the giant and $L_{\rm RE}$ represents the portion of the hot component luminosity, $L_{\rm h}$, impacting the giant. If the separation between the stars, A, is significantly larger than the giant's radius, $R_{\rm g}$, then $L_{\rm RE} = (R_{\rm g}/2A)^{2}\times L_{\rm h}$, and Eq. (1) reads as

\begin{displaymath}\Delta m_{\rm max} = - 2.5\log (1 + \beta /2),
\end{displaymath} (2)

where the parameter

\begin{displaymath}\beta=\frac{R_{\rm g}^{2}}{A^{2}}\frac{L_{\rm h}}{L_{\rm g}}
\end{displaymath} (3)

measures the strength of the illuminating radiation field relative to that of the giant. So the amplitude of the LC caused by the reflection effect is determined only by the parameter ${\beta }$. Because of its importance in defining the investigated amplitude we also determined its uncertainties in the cases under discussion (Appendix A). Results are summarized in Table 1. We can see that the parameter ${\beta }$ determined from observations can produce a maximum magnitude difference $\Delta m_{\rm max} < 0.1$mag, which is far below the observed quantities. On the other hand, the reflection effect (Eq. 2) requires $\beta \ge 1 - 10$ to match the observed amplitudes.
  \begin{figure}
\par\includegraphics[width=8cm]{ms9660f2r.eps} \end{figure} Figure 2: Profiles of LCs given by the reflection function for inclination of the orbit $i=90^{\circ }$ and $45^{\circ }$ and limb darkening coefficient u=0.6. They are characterized by the parameter $a \mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hfil
$\displaystyle ... (Sect. 3.2)

However, this problem should be treated by solving the radiation transfer of a very hot light ( $T_{\star} \sim 10^{5}\,{\rm K}$) throughout a very cool atmosphere ( $T_{\rm eff} \sim 3\,000\,{\rm K}$) to learn how the reprocessed UV/EUV radiation contributes into the Balmer and Paschen continua. An exact approach to the reflection effect was outlined by Vaz & Nordlund (1985) and Nordlund & Vaz (1990) for similar effective temperatures of the component stars, but not for very cool stars, where the TiO absorption bands are important. Recently, Proga et al. (1996) treated this problem for symbiotic binary stars using a non-LTE photoionization model, but also without including molecules. According to their model, significant changes in the structure of the red giant atmosphere are expected for $\beta \gg $ 1 and negligible when $\beta \ll $ 1. Their calculations showed that the magnitude difference between the illuminated and non-illuminated hemisphere $\Delta K \mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hfil
$\displa...
...neskip\halign{\hfil$\scriptscriptstyle ...mag in the range of considered temperatures between 20000 and 200000K for ${\beta }$ = 10, 1, 0.1 and 0.01 (cf. their Fig. 6). Also according to this study, the theoretical differences in broadband magnitudes between the opposite hemispheres of an illuminated red giant are also very small, $\sim0.0 - 0.1$mag, far from those observed.

3.2 The shape of light curves

To characterize the shape of the observed LC we introduce a parameter a as

\begin{displaymath}a = \frac{m(0) - m(0.25)}{\Delta m_{\rm max}},
\end{displaymath} (4)

where m(0) and m(0.25) are the magnitudes at the orbital phases 0 and 0.25, respectively, and $\Delta m_{\rm max}$ is the amplitude of the LC. The shape of the LC resembles a sinusoidal curve for a = 0.5, but a > 0.5 implies a broader maximum than minimum. We can recognize 3 types of LCs, characterized by (i) $a \sim 0.5$ (e.g. V1329Cyg, AGPeg, left panels of Fig. 1), (ii) 0.5 < a < 1 (e.g. CICyg, AXPer, mid panels of Fig. 1) and (iii) $a \approx 1$ (e.g. He2-467, EGAnd, right panels of Fig. 1). In some cases the parameter a depends on wavelength: $a_V > a_B \mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hfil
$\displ...
...\offinterlineskip\halign{\hfil$\scriptscriptstyle ... (Table 1). Note that extreme values of $a \sim $1 indicate the possible presence of a secondary minimum in the LC.

Shaping of LCs caused by the reflection effect is determined by a reflection function. To construct such a LC we assume that the observed luminosity of the binary, $L(\epsilon)$, is given by the sum of a constant part of the system luminosity, $L_{\rm const}$, given mainly by stellar components, and a phase dependent variable light, $L_{\rm v}(\epsilon)$, given by the reflection function. Then we can write

\begin{displaymath}L(\epsilon) = L_{\rm const} + L_{\rm v}(\epsilon),
\end{displaymath} (5)

where $\epsilon = \arccos(\sin i \cos\theta)$ is the angle between the line of sight and the direction to the hot component, the phase angle $\theta$ is determined by the position of the hot star on its relative orbit around the cool giant and i is the orbital inclination. The observed magnitude of the system then can be expressed as

\begin{displaymath}m(\epsilon) = - 2.5\log\left[1+\frac{L_{\rm v}(\epsilon)}{L_{\rm const}}
\right]+m_{\rm const}.
\end{displaymath} (6)

In our calculations we adopted the reflection function derived by Hadrava (1992). Figure 2 shows example of LCs given by Eq. (6). We can see that the reflection effect produces a strictly periodic modulation of the light along the orbital cycle characterized by the parameter $a \mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hfil
$\displaystyle .... Therefore the observed profiles characterized with $0.5 < a \mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hfil
$\display...
...r{\offinterlineskip\halign{\hfil$\scriptscriptstyle ... cannot be reproduced by the reflection effect. In addition, recently revealed systematic variation in the minima positions in the LCs of symbiotic binaries (Skopal 1998a) also argues against the location of the main source of the optical continuum on the giant's hemisphere.

We conclude that the observational characteristics of the LCs of symbiotic binaries - the large amplitude, the profile of minima and variation in their positions - cannot be reproduced by the reflection effect.

4 What mimics the reflection effect in symbiotic binaries?

To get a better idea of the origin of the orbitally related wave-like variation we discuss it within the basic model of symbiotic binaries - the cool giant losing material via the stellar wind and the hot luminous compact object ionizing a portion of the neutral wind. Such composition creates a strong source of nebular emission in the binary, which often dominates the optical region (e.g. BFCyg, AG Dra, He2-467, AS338). Therefore we discuss the apparent variation in the optical continuum within an ionization model.

First, we introduce the simplest model of the ionization structure in symbiotic binaries.

4.1 A zero level ionization model


 

 
Table 2: Observed and calculated EM for selected objects
Object $F_{\lambda}^{\rm obs}/10^{-13}$ Ref. $\int_{V}n^{2}{\rm d}V$ (Eq. 9) $L_{\rm ph}/\alpha_{B}$ (Eq. 10) $\int_{V}n^{2}{\rm d}V$ (Eq. 13) $\int_{V}n^{2}{\rm d}V^{c}$
  [ergcm-2s-1Å-1]   [cm-3] [cm-3] [cm-3] [cm-3]
ZAnd 7.5a 1 3.4 $\; 10^{59}$ 2.9 $\; 10^{59}$ 1.7 $\; 10^{59}$  
ZAnd 2.4 - 9.6b Fig. 1 $1.9 - 7.5\; 10^{59}$     $1.9 - 6.0\; 10^{59}$
BFCyg 5.0a 2 3.8 $\; 10^{60}$ 2.9 $\; 10^{60}$ d  
BFCyg 2.7 - 7.9b Fig. 1 $3.6 - 10\; 10^{60}$     $2.6 - 5.3\; 10^{60}$
AGDra 2.4 a 3 1.5 $\; 10^{59}$ 1.5 $\; 10^{59}$ 1.1 $\; 10^{59}$  
AGDra 0.9 - 2.2b Fig. 1 $0.5 - 1.3\; 10^{59}$     $3.5 - 8.0\; 10^{58}$
AXPer 2.0a 4 2.1 $\; 10^{59}$ 1.2 $\; 10^{59}$ d  
AXPer 1.0 - 2.5b Fig. 1 $1.8 - 4.6\; 10^{59}$     $1.6 - 5.5\; 10^{59}$
V443Her 2.1a 5 3.0 $\; 10^{59}$ 4.2 $\; 10^{59}$ 1.9 $\; 10^{59}$  
V443Her 1.1 - 2.1b Fig. 1 $2.7 - 5.2\; 10^{59}$     $1.0 - 2.0\; 10^{59}$

a - from the energy distribution in the spectrum at $\lambda$3646-Å.
b - from the dereddened U-magnitude at minimum and maximum, respectively:
ZAnd: U = 12.3 - 10.8, EB-V = 0.35, d = 1.12kpc, BFCyg:
U = 12.4 - 11.3, EB-V = 0.4, d = 4.6kpc, AGDra: U = 12.0 - 11.0, EB-V = 0.05,
d = 1.0kpc (Appendix A), AXPer: U = 12.9 - 11.9, EB-V = 0.27, d = 1.73kpc, V443Her: U = 12.2 - 11.5, EB-V = 0.15, d = 2.0kpc.
c - the range of the observed EM referred in the literature. d - not applicable.
Ref.: 1 - Fig. 1 of Fernández-Castro et al. (1988), 2 - Fig. 3b of Fernández-Castro et al. (1990), Skopal et al. (1997),
3 - Fig. 3 of Mikolajewska et al. (1995), Appendix A, 4 - Fig. 2 of Mikolajewska & Kenyon (1992), Skopal (2000), 5 - Fig. 1 of Dobrzycka et al. (1993).



  \begin{figure}
\par\includegraphics[width=8cm]{ms9660f3r.eps} \end{figure} Figure 3: The Hi/Hii boundary calculated for X = 0.3, 1, 10, the stellar wind model characterized by the parameters $\gamma $ = 2.5 and $R_{\rm g}/A$ = 0.28

The extent of the ionized zone can be obtained from a parametric equation

\begin{displaymath}f(r,\vartheta) - X = 0,
\end{displaymath} (7)

the solution of which defines the boundary between neutral and ionized gas at the orbital plane determined by a system of polar coordinates, $r,\,\vartheta$, with the origin at the hot star. The function $f(r,\,\vartheta)$ was treated for the first time by Seaquist et al. (1984), hereafter STB, for a steady state situation and pure hydrogen gas. The parameter X is given mainly by the binary properties - separation of the components, number of hydrogen ionizing photons, terminal velocity of the wind, $v_{\infty}$, and the mass-loss rate (for details see STB, Nussbaumer & Vogel 1987). The particle density of the ionized material is given by the velocity distribution of the giant's wind, which is assumed to be of the form

\begin{displaymath}v_{\rm wind} = v_{\infty}(1- R/r)^{\gamma},
\end{displaymath} (8)

where r is the distance from the centre of the cool star, and R is the origin of the stellar wind ($\approx $the radius of the giant). Figure 3 shows examples of the Hi/Hii boundary for X = 0.3, 1, 10 and the parameter $\gamma $ = 2.5 in the wind model (8). STB used $\gamma $ = 0, which represents a constant velocity of the wind (= $v_{\infty}$); no acceleration zone above the giant's photosphere exists. However, stellar wind characterized by the parameter $\gamma > 0$ will accelerate gradually above the photosphere to its terminal velocity; it is a more realistic model. Therefore, according to Schröder (1985), we adopted $\gamma $ = 2.5 in our calculations. In this model, the source of the nebular radiation is physically displaced from the cool giant photosphere.

We now test if the amount of emission produced by this model is consistent with observations.

4.2 Emission measure

We investigate the balance between the observed nebular emission in the continuum and that produced by the ionization model. The nebular flux largely depends on the number of hydrogen recombinations, and is proportional to $\int \!n_{+}n_{\rm e}\,{\rm d}V$, (the so called emission measure - EM); n+ and $n_{\rm e}$ is the concentration of ions (protons) and electrons, respectively.

(i) Observations: The quantity of the EM can be estimated, for example, from the measured flux, $F^{\rm obs}_{\lambda}$ ( $\rm erg\,cm^{-2}\,s^{-1}\,\AA^{-1}$), of the nebular continuum at the wavelength $\lambda$, according to the equation

\begin{displaymath}4\pi d^{2} F^{\rm obs}_{\lambda} = \varepsilon_{\lambda}\!\int_{V}\!\!
n_{+}n_{\rm e}\,{\rm d}V,
\end{displaymath} (9)

in which d is the distance to the object, $\varepsilon_{\lambda}$ is the volume emission coefficient per electron and per ion ( $\rm erg\,cm^{3}\,s^{-1}\,\AA^{-1}$) and V is the volume of the ionized zone. The nebular flux can be obtained from the energy distribution in the spectrum. Its upper limit can also be estimated from the dereddened U-magnitude of systems, in which the nebular continuum dominates the optical.

(ii) Model: The source of the nebular radiation in the model is the ionized region, in which the rate of ionization/recombination processes is balanced by the rate of photons, $L_{\rm ph}$ (photonss-1), capable of ionizing the element under consideration. In the case of pure hydrogen we can write the equilibrium condition as

\begin{displaymath}L_{\rm ph} = \alpha_{B} \!\int_{V} \!\!n_{+}(r)n_{\rm e}(r)\,{\rm d}V,
\end{displaymath} (10)

where $\alpha_{B}$ ( $\rm cm^{3}\,s^{-1}$) is the total hydrogenic recombination coefficient. The number of hydrogen ionizing photons, $L_{\rm ph}$ is

\begin{displaymath}L_{\rm ph}= \frac {L_{\rm h}}{\sigma T_{\star}^{4}}\pi (hc)^{...
...{912}_{0}\!\! \lambda B_{\lambda}(T_{\star})\,{\rm d}\lambda ,
\end{displaymath} (11)

where $L_{\rm h}$[ergs-1] and $T_{\star}$ is the total luminosity and the temperature of the hot star, respectively. Having independently determined $L_{\rm ph}$ we compare the EM given by observations (Eq. 9) and that required by the ionization model (Eq. 10). In Table 2 we give results for the objects with available parameters. We obtained the observed fluxes from the energy distribution in the spectrum at $\lambda 3646^{-}$Å and used the hydrogen emission coefficient $\varepsilon_{3646^{-}} =
3.36\; 10^{-28}\,\,\rm erg\,cm^{3}\,s^{-1}\,\AA^{-1}$ (Gurzadyan 1997). For a comparison, we also estimated the nebular flux from the U-magnitude according to the calibration of Henden & Kaitchuck (1982). In this case we adopted $\varepsilon_{U} =
1.9\; 10^{-28}\,\,\rm erg\,cm^{3}\,s^{-1}\,\AA^{-1}$ as the average of $\varepsilon_{3646^{-}}$ and $\varepsilon_{3646^{+}}$.

We can calculate the EM directly by integrating emission contributions throughout the volume of the ionized zone defined by the model (Eq. 7). The calculation of the Hi/Hii and Hei/Heii boundary in 2-D representation can be found in STB and Nussbaumer & Vogel (1987), respectively. Using Nussbaumer & Vogel (1989), we derive an upper limit to the modeled EM assuming the sphere around the cool star to be fully ionized from r = Q to $r = \infty$. The parameter Q is the location of the Hi/Hii boundary on the line joining the cool and the hot star ( $Q > R \sim R_{\rm g}$). The particle density n(r) is given by the mass-loss rate of the wind

\begin{displaymath}\dot M=4\pi r^{2}\mu m_{\rm H}n(r)v_{\rm wind},
\end{displaymath} (12)

where $\mu$ is the mean molecular weight, $m_{\rm H}$ is the mass of the hydrogen atom and the velocity of the wind is given by Eq. (8). Then the EM for a completely ionized medium ($n_{\rm e}$ = n+) can be calculated from the following analytical expression

\begin{displaymath}\int_{V} \!\!n(r)^{2}\,{\rm d}V =
4\pi\Big[\frac{\dot M}{4\...
...int_{Q}^{\infty}\!\!
\frac{{\rm d}r}{r^{2}(1-R/r)^{2\gamma}} \end{displaymath}


\begin{displaymath}=4\pi\Big[\frac{\dot M}{4\pi\mu {\rm m}_{\,\rm H}
v_{\infty...
...ma)}
\Big[1-\Big(1-\frac{R}{Q}\Big)^{1-2\gamma}\Big]\nonumber
\end{displaymath}

for $\gamma \ne~ 0.5$
and

\begin{displaymath}= - 4\pi\Big[\frac{\dot M}{4\pi\mu {\rm m} _{\rm H}
v_{\inft...
...\frac{R}{Q}\right)
\hspace*{0.5cm} {\rm for}~~\gamma~ =~ 0.5.
\end{displaymath} (13)

Nussbaumer & Vogel (1989) derived formula (13) for the special case of $\gamma $ = 2.5. This approximation can be used for cases when the major part of the circumbinary environment is ionized, i.e. the parameter X > 10 (Fig. 3). We applied the formula (13) to ZAnd, AGDra and V443Her (Col. 6 in Table 2). The calculated EM is somewhat lower than that indicated by observations. However, given the large uncertainties in fundamental parameters (mainly in d, $\dot M$ and $L_{\rm h}$, see Appendix A) we still consider the calculated values to be consistent with observations. However, if the calculated EM according to Eq. (13) is really lower than that measured, this could imply the presence of an additional source of particles in the system - for example, the hot star wind. Note that in the case of an open ionized zone a portion of the $L_{\rm ph}$ photons escapes the system, and thus an injection of new particles (emitters) into such a zone will produce an extra flux.

We find that the observed EM is consistent with that produced by the ionization model. This implies that all the $L_{\rm ph}$ photons consumed by the particles of the giant wind are needed to produce the observed nebular flux. However, in the model of the reflection effect only a small part of ionizing photons, $(R_{\rm g}/2A)^{2}\times L_{\rm ph}$ (Sect. 3), can be used to produce the nebular radiation. This causes the discrepancy between the ${\beta }$ parameter given by observations and much larger value, required by models of reflection effect to explain the amplitude of the LCs.

We now will demonstrate that the variation in the EM is responsible for the investigated wave-like variation in the LCs.

4.3 Variation in the emission measure

The quantity of the EM in the continuum also varies as a function of the orbital phase (e.g. Fernandez-Castro et al. 1988; Mikolajewska et al. 1989; Mikolajewska & Kenyon 1992; Dobrzycka et al. 1993). To investigate this variability we express Eq. (9) in the scale of magnitudes ( $m_{\lambda}=-2.5\log(F_{\lambda})+q_{\lambda}$) as

\begin{displaymath}m_{\lambda} = -2.5\log(EM) + C_{\lambda},
\end{displaymath} (14)

where

\begin{displaymath}C_{\lambda} = q_{\lambda} - 2.5\log\left(\frac{\varepsilon_{\lambda}}
{4\pi d^{2}}\right),
\end{displaymath} (15)

in which the constant $q_{\lambda}$ defines magnitude zero. For the standard photometry and fluxes in units of $\rm erg\,cm^{-2}\,s^{-1}\AA^{-1}$, qU = -20.9, qB = -20.36 and qV = -21.02 (Henden & Kaitchuck 1982). Using Eq. (14) we constructed the LCs from the measured values of the EM in BFCyg and ZAnd and compared them to those obtained photometrically. We calculated the B-magnitudes, because in these objects the nebular contribution still dominates the continuum and the emission coefficient is nearly constant in this region. We used $\varepsilon_{B} =
0.5~ 10^{-28}\,\rm erg\,cm^{3}\,s^{-1}\,\AA^{-1}$ (Gurzadyan 1997) and d = 4.6 and 1.12kpc for BFCyg and ZAnd, respectively. Figure 4 shows that the variation in the EM follows well that observed in the LCs. In other systems, where only a few measurements of the EM at different orbital phases are available (AXPer, AGDra, V443Her), we estimated the amplitude as

\begin{displaymath}\Delta m_{EM} = -2.5\log\frac{EM_{\rm min}}{EM_{\rm max}}\cdot
\end{displaymath} (16)

We find that the observed range of the EM is comparable with the amplitude of LCs in the U band of these systems (the last column in Table 2). We conclude that the variation in the EM produces the observed phase-dependent variation in the LCs of symbiotic binaries.

Note that the decrease of the LC amplitude with wavelength is caused by an increase of the cool giant contribution, which does not vary with the orbital phase. The same effect takes place towards the short wavelengths due to an increase in the stellar contribution from the hot star (see Fig. 4 of Kenyon et al. 1993).

  \begin{figure}
\par\includegraphics[width=7.3cm]{ms9660f4ar.eps} \includegraphics[width=7.3cm]{ms9660f4br.eps} \end{figure} Figure 4: Top: variation in the EM of BFCyg as a function of the orbital phase. The data (Mikolajewska et al. 1989) were converted into the B-magnitudes according to Eq. (14). Compared is the LC in the B band obtained photometrically during the same period, between JD 2445700 and 2446718 (Hric et al. 1993). Bottom: the same as the top, but for ZAnd. Measurements of the EM were taken from Fernandez-Castro et al. (1988), and photometric B-magnitudes from Fig. 1, but omitting the active phase. These results show that the variation in the EM is fully responsible for the variation in the LCs

4.4 Variation in the hydrogen lines

Together with the periodic variation in the nebular continuum, the same type of variability is observed in fluxes of Balmer lines. The source of hydrogen emission in lines is also the Hii region. Therefore the variation in both the hydrogen continuum and the lines should be of the same nature. So the EM derived from the hydrogen continuum should be consistent with that given by the Balmer lines, assuming an optically thin regime and the case B of recombination. In Table 3 we summarize results for the line H${\beta }$.

 

 
Table 3: Emission measure in the line H${\beta }$ for selected objects
Object $F_{\beta}/10^{-12}$a Ref. $EM_{\beta}$
  [ergcm-2s-1]   [cm-3]
ZAnd 37.3 1 4.5 $\; 10^{58}$
BFCyg 18 - 65 2 0.4 $- 1.3\; 10^{60}$
AGDra 6.4 - 9.4 3 6.2 $- 9.1\; 10^{57}$
AXPer 7.2 - 22 4 2.1 $- 6.3\; 10^{58}$
V443Her 6.5 - 15 5 2.5 $- 5.7\; 10^{58}$
a - dereddened fluxes with EB-V referred in Table 2.
Ref.: 1 - Mikolajewska & Kenyon (1996), 2 - Mikolajewska et al. (1989),
3 - Mikolajewska et al. (1995), 4 - Mikolajewska & Kenyon (1992), 5 - Dobrzycka et al. (1993).


We calculated the $EM_{\beta}$ according to Eq. (9) using the volume emission coefficient in the H${\beta }$ line, $\varepsilon_{\beta} = 1.23\; 10^{-25}$ergcm3s-1. We can see that the $EM_{\beta}$ is by a factor of $\sim$5, on average, lower than that derived from the Balmer continum. This discrepancy can be caused by atenuation of the Hi emission due to (i) an absorption originating from the cool component wind and (ii) the self-absorption effect, when the nebula is partially opaque in the line H${\beta }$ and H$\gamma $, in addition to the case B. The first case is demonstrated well by sets of observations along the orbital cycle (e.g. Oliversen et al. 1985). The wind absorption component is more pronounced around the inferior conjunction of the giant (see Fig. 3), which makes the amplitude of the variation in line fluxes even larger. The second case is indicated by the observed very steep Balmer decrement (H${\alpha}$/H${\beta }$/H$\gamma $ $\approx $ 7/1/0.4, for objects in Table 3), which is not consistent with the theoretical prediction (2.85/1/0.47) that the excitation is due to photoionization. Moreover, attenuation of hydrogen fluxes could also be in part due to electron collisions in a dense Hii region, and/or partly caused by selective interstellar absorption. Therefore the $EM_{\beta}$ represents only the lower limit of the EM derived from the Balmer continuum.

As the variation in the emission of the Balmer lines is connected with the Hii region - the dominant source of the optical/near-UV continuum - the observed periodic wave-like variation in the continuum should always be followed by a similar variation in Balmer lines.

4.5 Why does the emission measure vary?

To produce the wave-like variation in the LCs along the orbital cycle, the nebula - the main source of the optical continuum in symbiotic binaries - has to be partially optically thick and of a non-spherical shape. In our simple ionization model the opacity, $\kappa$, of the ionized emission medium decreases with the distance from the cool star, since $\kappa \propto n \propto r^{-2}$ (i.e. its parts nearest to the giant's surface will be most opaque). It is probable that the observed emission will also depend on the extension of the ionized region. Below we give a qualitative description on how, or whether, it is possible to produce the observed profile of LCs within the ionization model mentioned above.

(i) In the case of an oval shape of the Hii zone (Fig. 3; a small parameter X), its total emission will be atenuated more at positions of the inferior and superior conjunction of the cool star (the orbital phase $\varphi$ = 0 and 0.5, respectively) than at positions of $\varphi$ = 0.25 and 0.75, respectively. Such apparent variation in the EM will produce both the primary and the secondary minimum in the LC and will thus mimic the ellipsoidal effect in binaries containing a giant star. This type of LC profile corresponds to the parameter $a \sim 1$ (right panels of Fig. 1).

(ii) A gradual opening of the Hii zone (approximately $0.3 < X \mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hfil
$\display...
...r{\offinterlineskip\halign{\hfil$\scriptscriptstyle ...) will make it optically thinner behind the hot star (outside the binary around $\varphi$ = 0.5). Thus, more of the nebular radiation, relative to the case (i), will be observed at the position of $\varphi \sim 0.5$. The secondary minimum in LCs will therefore become less pronounced or flat, and/or a maximum at $\varphi \sim 0.5$ can arise. The LC profile here should be characterized by the parameter a > 0.5 (mid panels of Fig. 1).

(iii) Given an extensive emission zone (X > 10) one can imagine the partially optically thick portion of the Hii region as a cap on the Hi/Hii boundary around the binary axis. This resembles the geometry of the reflection effect, but the emission region causing the light variation is physically displaced from the giant's surface (see also a sketch in Baratta & Viotti (1990), who drawn such regions for Feii and Ciii lines). In these cases the LC profile is similar to that of the reflection effect, i.e. the parameter $a \le 0.5$ (left panels of Fig. 1).

A relationship between the parameters a and X supports the connection between the shape of the LC and the extent of the symbiotic nebula mentioned above (Fig. 5, Appendix B).

However, the real structure of the ionized region in symbiotic binaries is probably much more complex. Currently it is being intensively investigated (e.g. Schmid 1998). For example, the observed systematic variation in the minima position (i.e. an apparent change of the orbital period) requires an asymmetrical shape of the Hii zone with respect to the binary axis (see Sect. 4.1 of Skopal 1998a in more detail). A modification of the STB model, which includes effects of the orbital motion, is outlined in Appendix C.

5 Conclusion

We find that:

1.
The observed properties of the orbitally related variation in the LCs of symbiotic binaries - the large amplitude, shaping of minima and systematic changes in their positions - cannot be produced by the reflection effect.
2.
According to the basic ionization model of symbiotic binaries, the main source of the optical continuum is the nebula, which arises from ionization of the cool giant wind by the hot star radiation. We found that:
(a)
The observed EM is consistent with that produced by the ionization model.
(b)
Variation in the EM is fully responsible for the observed wave-like modulation of the LCs of symbiotic binaries with the orbital phase.
(c)
The variation in the optical continuum should always be followed by a similar variation in Balmer lines.
3.
To explain the orbitally-related variation, the nebula has to be partially optically thick and of a non-symmetrical shape to produce different contributions of its total emission into the line of sight at different orbital phases.
4.
The LC profile depends on the extent of the symbiotic nebula. Large nebulae ( $X \mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hfil
$\displaystyle ...) produce a sinusoidal LC ( $a \sim 0.5$). Less extended nebulae ( $X \mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hfil
$\displaystyle ...) have a flatter LC at its maximum, and/or create a secondary minimum, ( $0.5 < a \mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hfil
$\display...
...r{\offinterlineskip\halign{\hfil$\scriptscriptstyle ...), which mimics the ellipsoidal effect.

Acknowledgements
This research has been supported by the Slovak Academy of Science under a grant No. 5038/2000 and the Alexander von Humboldt foundation under project No. SLA/1039115. The author would like to thank his anonymous referee for constructive comments that allowed him to improve the original version of the present work.

References

 

6 Online Materiel

Appendix A:

The ${\beta }$ parameter (Eq. 3) is defined by the luminosity ratio $L_{\rm h}/L_{\rm g}$ and the giant radius in units of the separation of the components, $R_{\rm g}/A$. To determine these quantities we used published parameters and/or made appropriate estimates. If applicable, we used spectral types of the cool components in symbiotic binaries of Mürset & Schmid (1999) and empirically determined dependencies of effective temperature and linear radius upon the spectral type given by van Belle et al. (1999). Table 4 summarizes the resulting parameters. Their uncertainties represent mean square errors of the mean value given by Eq. (3). A brief explanation to Table 4 is given below for individual objects.
AXPer: Skopal (1994) determined $R_{\rm g}/A = 0.28 \pm 0.01$. The luminosity of the giant, $L_{\rm g} = 1\,250 \pm 400~L_{\odot}$ for the distance $d = 1\,730 \pm 230$pc (Skopal 2000). The hot star luminosity, $L_{\rm h} = 314 \pm 84~L_{\odot} (d/1730\,pc)^{2}$ (Mürset et al. 1991) with the uncertainty resulting from that of d.
BFCyg: Parameters $R_{\rm g}/A = 0.54 \pm 0.02$ and $L_{\rm h}/L_{\rm g} \approx 1.4$ (Skopal et al. 1997). The uncertainty of the luminosity ratio is $\sim$30%, which is relevant to its determination from the observed fluxes.
CICyg: Kenyon et al. (1991) estimated $R_{\rm g}/A = 0.38 \pm 0.02$. Adopting their estimate of the total mass of the binary, $M_{\rm T} = 1.9 \pm 0.6~M_{\odot}$, we get A = $470 \pm 50~R_{\odot}$ for $P_{\rm orb}$ = 855.25 days (Aller 1954), which yields $R_{\rm g} = 179 \pm 20~ R_{\odot}$. The spectral type (ST) of the red giant in CICyg, M5.5, corresponds to its effective temperature, $T_{\rm eff} = 3\,400 \pm 30$K, which then yields $L_{\rm g} = 3\,830 \pm 990~L_{\odot}$. Finally, Mürset et al. (1991) determined $L_{\rm h} = 560~L_{\odot}$(d/1.5kpc)2.
EGAnd: From the contact times of a minimum observed in continuum fluxes at $\lambda$1320Å (Pereira 1996) we determined $R_{\rm g}/A = 0.32 \pm 0.05$ for the orbital period, $P_{\rm orb}$ = 482 days (Skopal 1997) and a circular orbit. As the minimum is caused by Rayleigh scattering of the hot star radiation on the neutral atoms of the cool giant wind, this is an upper limit. The luminosity ratio for the two stars, $L_{\rm h}/L_{\rm g} \approx 1/60$ (Vogel et al. 1992). The uncertainty of this ratio is assumed to be of 30%.
AGDra: From the energy distribution in the spectrum during quiescence (Greiner et al. 1997) we estimated the observed fluxes $F^{\rm obs}_{\rm g} = 9.5 \pm 2.0 \; 10^{-9}$ and $F^{\rm obs}_{\rm h} = 1.3 \pm 2.0 \;
10^{-8}$ergcm-2s-1, i.e. $L_{\rm h}/L_{\rm g} = 1.3 \pm 0.3$. Smith et al. (1996) estimated the surface gravity as $\log(g) = 1.6 \pm 0.3$ (g in units of cms-2), which for the cool component mass of 1.5 $M_{\odot}$ (Mikolajewska et al. 1995), yields $R_{\rm g} = 32 \pm 11~R_{\odot}$. This value is also consistent with that corresponding to the recent $ST/T_{\rm eff}$ dependencies. For $M_{\rm T} = 2~M_{\odot}$ and $P_{\rm orb}$ = 550 days (Gális et al. 1999) we have $A = 356~R_{\odot}$ and thus $R_{\rm g}/A = 0.09 \pm 0.03$. We can also estimate the distance to AGDra $d = 980 \pm 200$pc from $L_{\rm g} = 285 \pm 100~ L_{\odot}$ ( $T_{\rm eff} = 4\,200\,\rm K$ as for K3-4III giant) and $F^{\rm obs}_{\rm g}$.
V1329Cyg: The maximum width of the pre-outburst eclipses (Fig. 1 of Schild & Schmid 1997),

 

 
Table A.1: The ${\beta }$ parameter characterizing the reflection effect
Object $L_{\rm h}/L_{\rm g}$ $R_{\rm g}/A$ ${\beta }$
AXPer $0.25\pm 0.10$ $0.28\pm 0.01$ $0.020\pm 0.008$
BFCyg $1.4\pm 0.4$ $0.54\pm 0.02$ $0.40\pm 0.12$
CICyg $0.15\pm 0.06$ $0.38\pm 0.02$ $0.06\pm0.01$
EGAnd $0.017\pm0.005$ $\le 0.32\pm0.05$ $\le 0.002\pm0.001$
AGDra $1.3\pm0.3$ $0.09\pm 0.03$ $0.01\pm0.008$
V1329Cyg 3.1-1.2 <0.39 0.18 - 0.47
He2-467 $\approx $60 0.05-0.03 0.07 - 0.2
ZAnd $\mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hfil
$\displaystyle ...1 $0.24\pm0.05$ $\mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hfil
$\displaystyle ...
V443Her $\sim$0.7 $\sim$0.26 $\sim$0.04
AGPeg $\sim$1 $\sim$0.17 $\sim$0.03


t4 - t1 = 0.129 $P_{\rm orb}$, yields the upper limit of $R_{\rm g}/A$ = 0.39 (assuming the radius of the eclipsed object to be negligible) for $P_{\rm orb}$ = 958 days (Schild & Schmid 1997). Mürset et al. (1991) derived $L_{\rm h} = 9\,500~L_{\odot}$. The ST of the giant in V1329Cyg, M6, corresponds to $T_{\rm eff} = 3\,375 \pm 100$K. A reasonable range of $M_{\rm T} = 1 - 4~M_{\odot}$ (elements of the spectroscopic orbit are not available) gives the range of $A = 410 - 650\,R_{\odot}$, consequently $R_{\rm g} = 160 - 260~R_{\odot}$ and $L_{\rm g} = 3\,100 - 7\,800~L_{\odot}$. Thus for V1329Cyg we can estimate only a range of the ${\beta }$ parameter.
He2-467: From the energy distribution in the spectrum (Munari & Buson 1992) we estimated the luminosity ratio $L_{\rm h}/L_{\rm g} \approx 60$ (assuming that the observed nebular component is equal to $\int_{0}^{912}F_{\rm h}(\lambda)\,{\rm d}\lambda$), and particularly $F^{\rm obs}_{\rm g}
= 6.3 \pm 2.0 \; 10^{-10}$ergcm-2s-1, which gives $L_{\rm g} = 78 \pm 20~L_{\odot}$. This value is in a very good agreement with the $ST/T_{\rm eff}/R$ dependencies (ST = K0III: $T_{\rm eff} = 4\,513 \pm 100$K, $R_{\rm g} = 14 \pm 3~R_{\odot}$ that implies $L_{\rm g} = 73 \pm 25~L_{\odot}$). To estimate the separation A, we assume a typical range of $M_{\rm T} = 1 - 4~M_{\odot}$, which for $P_{\rm orb} = 478.5$ days (Arkhipova et al. 1995) corresponds to the range of $A = 257 - 408~R_{\odot}$.
ZAnd: For the spectral type of the giant in ZAnd, M4.5III, the $ST/T_{\rm eff}/R$ and V-K/R dependencies suggest $T_{\rm eff}$ = 3425K, $R_{\rm g} = 100\pm 20~R_{\odot}$ implying $L_{\rm g} = 1\,230~L_{\odot}$. We used the V-K = 5.4 (Kamath & Ashok 1999, Fig. 1, EB-V = 0.3). According to Schmid & Schild (1997) $M_{\rm T} = 1.8~M_{\odot}$, which for $P_{\rm orb}$ = 758.8 days (Mikolajewska & Kenyon 1996) yields $A = 420~ R_{\odot}$, and Mürset et al (1991) derived $L_{\rm h} = 700 \pm 50~L_{\odot}~(d/1.2\,kpc)^{2}$. So in ZAnd we have $R_{\rm g}/A = 0.24 \pm 0.05$ and $L_{\rm h}/L_{\rm g} \mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hf...
...r{\offinterlineskip\halign{\hfil$\scriptscriptstyle ... for the range of possible distances (0.98 - 1.6kpc, Mürset et al. 1991). This luminosity ratio is also supported by the energy distribution in the spectrum of ZAnd (e.g. Nussbaumer & Vogel 1989).
V443Her: Only rough estimates of fundamental parameters are available in the literature: $L_{\rm g} \sim 1\,500~L_{\odot}$, $L_{\rm h} \sim 1\,000~L_{\odot}$, $R_{\rm g} \sim 110~R_{\odot}$, $M_{\rm T} \sim 2.9~M_{\odot}$ (Dobrzycka et al. 1993). For $P_{\rm orb} = 594\pm 3$ days (Kolotilov et al. 1995) we get $A \sim 424~R_{\odot}$.
AGPeg: Kenyon et al. (1993) estimated $L_{\rm g} \sim 1\,150~L_{\odot}\,(d/0.8\,kpc)^{2}$ and Mürset et al. (1991) determined $L_{\rm h} \sim 1\,000~L_{\odot}\,(d/0.8\,kpc)^{2}$, i.e. $L_{\rm h}/L_{\rm g} \sim 1$. The $ST/T_{\rm eff}/R$ dependencies suggest $T_{\rm eff}$ = 3425K, which corresponds to $R_{\rm g} \sim 89~R_{\odot}(d/0.8\,kpc)^{2}$, and $M_{\rm T} \sim 3.1~M_{\odot}$ (Kenyon et al. 1993) implies $A \sim 530~R_{\odot}$ ( $P_{\rm orb}$ = 812.6 days, Skopal 1998a), and thus $R_{\rm g}/A \sim 0.17$.

Appendix B:

Here we investigate the suggested connection between the parameters a and X (Sect. 4.2). STB derived the parameter X as

\begin{displaymath}X=\frac{4\pi\mu^{2}m_{\rm H}^{2}}{\alpha_B}A L_{\rm ph}
\Big(\frac{v_{\infty}}{\dot M}\Big)^{2}.
\end{displaymath} (B.1)

The meaning of individual parameters is noted in the text above. Unfortunately, there are only a few symbiotic objects for which the parameter X can be satisfactorily determined. In Table 5 we summarize the average values of parameters $\dot M$ in $10^{-7}~M_{\odot}$ yr-1, $L_{\rm ph}$ in $10^{46}\,\rm photons\,s^{-1}$ (Eq. (11)), a (Eq. (4), Table 1) and X. Other auxiliary parameters as in Appendix A and in Mürset et al. (1991), if not referred to otherwise. In all cases $v_{\infty} = 30\,\rm km\,s^{-1}$.
  \begin{figure}
\par\includegraphics[width=6.6cm]{ms9660f5r.eps} \end{figure} Figure B.1: A correlation between the shape of the LC characterized by the parameter a (Sect. 3.2) and the extent of the symbiotic nebula given by the parameter X


 

 
Table B.1: Parameters a and X for selected objects
Object $\dot M$ Ref. $L_{\rm ph}$ a X
AGPeg 2.0   7.2 0.50 >15
ZAnd 2.0 1 3.5 0.53 $\approx $14
AGDra 2.0 2 2.6 0.50 11
V1329Cyg 15   56 0.50 $\sim$8
BFCyg $\approx $20   50 0.57 $\approx $3
CICyg >4   3.7 0.83 <5
AXPer $\sim$10 3 2.2 0.70 $\sim$0.4
EGAnd 2.0 4 0.077 1.0 0.3
Ref.: 1 - Fernández-Castro et al. (1988), 2 - Mikolajewska et al. (1995),
3 - Skopal et al. (in press), 4 - Vogel (1991): this value is needed to explain the nebular continuum.
In contrast, the value of 3-4 $\, 10^{-8}~M_{\odot}$ yr-1 suggested by effects of the Rayleigh scattering in the far UV continuum leads to X = 7.


The main obstacle to determining the X parameter results from its strong dependence on $\dot M$, which is very poorly known at present. The situation is difficult mainly in cases with small values of the parameter X, a little change in which produces a large change in the extent of the nebula. In addition, intrinsic variation in $\dot M$ and/or $L_{\rm ph}$ are often observed. For example, a variable column density of hydrogen atoms during different cycles of BFCyg (Fernandez-Castro et al. 1990) suggests a variability in the geometry of the Hii zone. Also the case of EGAnd is disputable (see Table 5) and for CICyg there is no detailed analysis of its current quiescent phase. In the latter case, possible values of $\dot M$ = $10^{-6}~M_{\odot}$ yr-1 and $v_{\infty} = 20\,\rm km\,s^{-1}$ result in X << 1 in contrast to its upper limit of 5 (Table 5). Therefore we adopted X = 1 for CICyg. On the other hand, all cases with very large X ( $\mathrel{\mathchoice {\vcenter{\offinterlineskip\halign{\hfil
$\displaystyle ..., AGPeg, ZAnd, AGDra,V1329Cyg) show a simple sinusoidal shape ( $a \sim 0.5$).

In spite of these problems the present knowledge of the fundamental parameters of symbiotic binaries makes a correlation between a and X possible (Fig. 5). However, further investigation is needed to determine more accurate parameters, mainly the mass-loss rate via the wind from cool giants in binaries, to verify the relationship between the profile of the LC and the extent of the symbiotic nebula.

Appendix C:

In this appendix we introduce a modification of the STB model accounting for the additional ionizations due to the inflow of neutral material into the ionized region through the ionization front due to the orbital motion and the velocity of the giant wind.

  \begin{figure}
\par\includegraphics[width=6.6cm]{ms9660f6r.eps} \end{figure} Figure C.1: The Hi/Hii boundary given by the STB model (dashed line) and its modification due to the orbital motion (solid line). Our model (Eq. C.1) was calculated for $P_{\rm orb}$ = 757 days, $A = 465~R_{\odot}$ and the mass ratio q = 6. The binary rotates anti-clockwise

At a boundary point, $r_{\rm b}$, the rate of particles, $n(r_{\rm b})v_{\perp}$, crosses the area of the front, dS = d $\Omega\,r^{2}/\cos(\textbf{\textit{r}}{\bf S})$, where d$\Omega$ is a small angle around the vector r pointing to $r_{\rm b}$ from the hot star and $v_{\perp}$ is the velocity of atoms in the direction of S (i.e. perpendicular to the boundary at the point $r_{\rm b}$). Thus, within the Hii region, the rate of photons, $L_{\rm ph}$, capable of ionizing hydrogen, has to balance a surplus of $\alpha_{B}[n(r_{\rm b})v_{\perp}]^{2} {\rm d}S$ recombinations in addition to the steady state situation; $\alpha_{B}$ stands for the total hydrogenic recombination coefficient for case B. The distance $r_{\rm b}$ from the hot star of the modified ionization front is then given by the equilibrium condition

\begin{displaymath}\frac{{\rm d}\Omega}{4\pi} L_{\rm ph}=\alpha_{B}\,{\rm d}\Ome...
...m d}r -
\alpha_{B}\,n^{2}(r_{\rm b})v_{\perp}^{2} {\rm d}S.
\end{displaymath} (C.1)

The velocity component, $v_{\perp}$, is calculated from the velocity of a particle ${\bf v = v_{\rm wind} - \omega \times \textbf{\textit{r}}_{\rm G}}$ in the frame rotating with angular velocity $\omega = 2\pi/P_{\rm orb}$; $\bf\textbf{\textit{r}}_{\rm G}$ is the position vector with respect to the centre of mass of the system. Figure 6 shows a comparison of the closed boundary calculated according to Eq. (C.1) and that of the STB model.


Copyright ESO 2001