KIC 9451096: Magnetic activity, flares and differential
rotation Revista mexicana de astronomía y astrofísica, vol. 54, no. 1, pp. 01-20, 2018 Instituto de Astronomía, UNAM
Abstract:
We present a spectroscopic and photometric analysis of KIC9451096. The combined
spectroscopic and photometric modelling shows that the system is a detached
eclipsing binary in a circular orbit and composed of F5V + K2V components.
Subtracting the best-fitting light curve model from the whole long cadence data
reveals additional low (mmag) amplitude light variations in time and occasional
flares, suggesting a low, but still remarkable level of magnetic spot activity
on the K2V component. Analyzing the rotational modulation of the light curve
residuals enables us to estimate the differential rotation coefficient of the
K2V component as k = 0.069 ± 0.008, which is 3 times weaker compared with the
solar value of k = 0.19, assuming a solar type differential rotation. We find
the stellar flare activity frequency for the K2V component as 0.000368411
h-1 indicating a low magnetic activity level.
Resumen:
Presentamos un análisis espectroscópico y fotométrico de KIC9451096. El modelo
combinado muestra que el sistema es una binaria eclipsante separada, en órbita
circular y compuesta de dos estrellas, F5V + K2V. Al sustraer la mejor curva de
luz modelada de la cadencia completa de datos se revelan pequeñas variaciones en
magnitud (mmag) así como ráfagas ocasionales, lo que sugiere una baja pero
notable actividad de manchas magnéticas en la componente K2V. El análisis de la
modulación rotacional de la curva de luz nos permite estimar que el coeficiente
de la rotación diferencial de la componente K2V es k = 0.069 ± 0.008, tres veces
más débil que l el valor solar, k = 0.19. Encontramos que la frecuencia de la
actividad de ráfagas en la K2V es 0.000368411 h-1, lo que indica una
baja actividad magnética.
1. Introduction
Although the primary aim of the Kepler mission is to detect
transiting planets by obtaining very high precision photometric measurements, it
provides further benefits, especially in terms of clear and reliable determination
of very small amplitude light variations on eclipsing and intrinsic variable stars.
About 150000 targets have been observed in the mission, and apart from the
exoplanets, numerous variable stars have been discovered. The unprecedented
precision of the Kepler photometry clearly revealed low amplitude
(mmag) light variations, which were used in the analysis of stellar flares, spot
activity and differential rotation (Balona
2015; Balona et al. 2016; Reinhold & Reiners 2013; Reinhold et al. 2013a). Among these variable
stars, 2876 eclipsing binary stars have been discovered (Prša et al. 2011; Slawson et
al. 2011). Careful light curve modelling of the binaries with cool
components (Teff < 6500 K) revealed rotational modulation of the light
curves and flares in model residuals. KIC 09641031 (Yolda ̧s & Dal 2016), KIC09761199 (Yolda ̧s & Dal 2017) and KIC2557430 (Kamil & Dal 2017), GJ1243, GJ 1245A and B (Hawley et al. 2014), KIC 2300039, KIC4671547 (Balona 2015) are examples of such stars.
The analyses of the patterns of magnetic activity exhibited by these stars reveal
some clues about their evolutionary stages. Although there are several indicators
found in these analyses, two of them are the energy spectra defined by Gershberg (1972) and the flare frequencies
described by Ishida et al. (1991). Both of
them have been computed, especially from the 1970’s to the 1980’s, in order to
figure out the magnetic activity levels for the stars with detected flares. In
1990’s, Leto et al. (1997) examined the flare
frequency variation of EV Lac, a well-known UV Ceti type star. There are a few
studies on the activity levels of three magnetic active stars discovered in the
Kepler Mission depending on their flare frequencies. Yolda ̧s & Dal (2016) detected 240 flares
from KIC09641031, and Yolda ̧s & Dal
(2017) detected 94 flares from KIC09761199. In addition, Kamil & Dal (2017) detected 69 flares from
KIC2557430. Yolda ̧s & Dal (2016) derived
the one phase exponential association (hereafter OPEA) model, and the flare
frequency N1 was found to be 0.41632 h-1 for KIC09641031.
Yolda ̧s & Dal (2017) computed
N1 as 0.01351 h-1 for 69 flares for KIC 09761199. However,
an interesting situation occurs in the case of KIC2557430. Kamil & Dal (2017) find that some of the flares detected
from KIC 2557430 come from a third body; it is unclear whether it is a component in
the system or an undetected background light source. Depending on the OPEA model
derived from 69 flares, Kamil & Dal
(2017) reveal that 40 (called Group 1) of them come from the secondary
component, while 29 flares (called Group 2) come from a third body. They computed
the flare frequency N1 as 0.02726 h-1 for Group 1 and 0.01977
h-1 for Group 2. As discussed by Yolda ̧s & Dal (2016) and Gershberg
(2005), the flare frequency is one of the parameters indicating the
nature of the flare mechanism in the stellar atmosphere. Apart from the classical
parameters described by Gershberg (2005),
Dal & Evren (2010, 2011) have also described some new parameters
derived from the OPEA models in order to determine the flare process occurring on
the stellar surface.
Continuous photometry of variable single stars discovered by Kepler
enabled to trace photometric period variations as a proxy of differential rotation
via Fourier transform (see, e.g. Reinhold et al.
2013b; Reinhold & Reiners
2013). However, the Fourier transform may not perfectly work in case of
eclipsing binaries, where the amplitude of the rotational modulation of star spots
is usually embedded into the relatively large amplitude light variations caused by
eclipses and the lack of spherical symmetry of the binary components. Furthermore,
insufficient representation of light curve models, especially around mid-eclipse
phases, may require discarding data around those phases and may cause regular gaps
in the light curve, which would lead to unwanted alias periods and harmonics. In
this case, alternative methods should be adopted to trace photometric period
variation, such as an O − C diagram based on minimum times of
rotationally modulated light curves (see, e.g. özdarcan et al. 2010).
In the case of eclipsing binary stars, additional intrinsic variations may not be
determined at first, due to the reasons explained above. KIC 9451096 is such an
eclipsing binary in the Kepler eclipsing binary catalog1 (Prša et al. 2011; Slawson et al.
2011) with a short period, and with a confirmed third body (Borkovits et al. 2016). Beyond the properties
provided by the catalog, such as morphology and eclipse depths, Armstrong et al. (2014) provided physical
information, estimated from the spectral energy distribution based on photometric
measurements. They estimated the effective temperature of the components of KIC
9451096 as 7166 K and 5729 K for the primary and the secondary component,
respectively.
In this study, we carry out a photometric and spectroscopic analysis of KIC 9451096,
based on Kepler photometry and optical spectroscopic observations
with intermediate resolution described in § 2. § 3 describes the spectroscopic and
photometric modelling of the system, and the analysis of the out-of-eclipse
variations. In the final section, we summarize and discuss our findings.
2. Observations and data reductions
2.1. Kepler Photometry
Photometric data obtained by the Kepler spacecraft cover a broad
wavelength range between 4100 ̊A and 9100 ̊A; this has the advantage of
collecting many more photons in a single exposure and reaching sub-milli-mag
precision, but also has the disadvantage of having no “true” photometric filter,
hence no photometric color information. There are two types of photometric data
having different exposure times. These are short cadence data (having an
exposure time of 58.89 seconds) and long cadence data (having an exposure time
of 29.4 minutes). In this study we use long cadence data of KIC 9451096 obtained
from the Kepler eclipsing binary catalog. The catalog provides
detrended and normalized intensities, which are obtained by application of
procedures described by Slawson et al.
(2011) and Prša et al. (2011).
The whole data covers ≈4 years of time, with 65307 data points in total. The
MAST archive reports 0.9% contamination level in the measurements, practically
indicating no additional light contribution to the measured fluxes of KIC
9451096.
2.2. Spectroscopy
We obtained optical spectra of KIC 9451096 with the 1.5 m Russian - Turkish
telescope equipped with the Turkish Faint Object Spectrograph Camera2 (TFOSC) at Tubitak National
Observatory. TFOSC enables one to obtain intermediate resolution optical spectra
inéchelle mode. In our case, the instrumental setup provides actual resolution
of R = λ/∆λ ≈ 2800 around 6500 ̊A, and the observed spectra cover a usable
wavelength range between 3900-9100 ̊A in 11 échelle orders. A back illuminated
2048 × 2048 pixels CCD camera, which has pixel size of 15 × 15 μm2,
was used to record spectra.
We obtained ten optical spectra of KIC9451096 during the 2014 and 2016 observing
seasons. In order to obtain enough signal, we used 3600 s of exposure time for
each observation. The estimated signal-to-noise ratio (SNR) of observed spectra
is mostly between 80-100, except for a few cases, where the SNR is around 50.
SNR estimation is based on photon statistic. Together with the target star, we
also obtained high SNR optical spectra of HD 225239 (G2V, vr = 4.80
km s-1) and ι Psc (HD 222368, F7V, vr = 5.656 km
s-1), and adopted them as radial velocity and spectroscopic
comparison templates.
We reduced all observations using standard IRAF3 packages and tasks. A typical reduction procedure
starts with obtaining a master bias frame from several bias frames taken
nightly, and subtracting the master bias frame from all object, calibration lamp
(Fe-Ar spectra in our case) and halogen lamp frames. Then the bias corrected
halogen frames are combined to form an average halogen frame and this average
frame is normalized to unity to produce the normalized master flat frame. After
that, all target and calibration lamp spectra are divided by the normalized flat
field frame. Next, cosmic rays removal and scattered light corrections are
applied to the bias and flat corrected frames. At the end of these steps,
reduced frames are obtained and these frames are used for the extraction of
spectra. In the final steps, Fe-Ar frames are used for wavelength calibration of
the extracted spectra and the wavelength calibrated spectra are normalized to
unity by using cubic spline functions.
3. Analysis
3.1. Radial Velocities and Spectroscopic Orbit
The first step of our analysis is to determine the radial velocities of the
components and the spectroscopic orbit of the system. We cross-correlated each
observed spectrum of KIC9451096 with spectra of template stars HD 225239 and ι
Psc, as described in Tonry & Davis
(1979). In practice we used the fxcor task in IRAF environment. We
achieved better cross-correlation signals (especially for the weak secondary
component) when we used HD 225239 as template; thus, we determined all radial
velocities with respect to the HD225239 spectrum. We obtained acceptable
cross-correlation signals of both components inéchelle orders 5 and 6, which
cover a wavelength range between 4900-5700 ̊A. Figure 1 shows the cross-correlation functions of two spectra
obtained around orbital quadratures.
Fig. 1 Cross-correlation functions of two spectra obtained around
orbital quadratures. The letter ϕ denotes
corresponding orbital phase. P and S indicate the primary component
and the secondary component, respectively.
We list the observation log and the measured radial velocities of the components
in Table 1. Note that we use the
ephemeris and period given by Borkovits et al.
(2016) and listed in their Table
2 to calculate orbital phases and for further analysis.
Table 1 Log of spectroscopic observations* *together with measured radial velocities and their corresponding
standard errors (σ) in kms−1.
HJD
Orbital
Exposure
Primary
Secondary
(24 00000+)
Phase
time (s)
Vr
σ
Vr
σ
56842.5435
0.7794
3600
91.4
8.2
-152.5
36.9
56844.4052
0.2682
3600
-79.9
6.3
151.9
39.1
56844.4479
0.3024
3600
-74.4
6.6
155.0
37.2
56889.4315
0.2781
3600
-77.1
5.7
148.1
40.0
56890.2958
0.9693
3600
14.5
5.0
-
-
57591.4532
0.7199
3600
88.5
7.2
-153.3
32.0
57601.4386
0.7058
3600
88.7
5.4
-149.8
32.1
57616.4778
0.7333
3600
86.0
4.3
-145.2
38.7
57617.5188
0.5659
3600
31.0
5.8
-
-
57672.3009
0.3779
3600
-54.8
5.1
111.1
47.9
Table 2 Spectroscopic orbital elements of KIC 9451096.
* *M1 and M2 denote the masses of the primary and the secondary
component, respectively, while M shows the total mass of the
system.
Parameter
Value
Porb (day)
1.25039069 (fixed)
T0 (HJD24 00000+)
54954.72942 (fixed)
(kms−1)
2.8±0.5
K1 (kms−1)
84.1±2.3
K2 (kms−1)
153.2±14.6
e
0 (fixed)
a sin i (R⊙)
5.92±0.35
M sin3 i (M⊙)
1.79±0.25
Mass ratio (q = M2/M1)
0.55±0.05
rms1 (kms−1)
3.7
rms2 (kms−1)
4.9
We achieved a reasonable solution for the spectroscopic orbit assuming zero
eccentricity, where an undefined longitude of periastron is taken. We checked
this assumption by inspecting the Kepler light curve of the
system, where we observe deeper and shallower eclipses at 0.0 and 0.5 orbital
phases, respectively, indicating a circular orbit (see § 3.3, Figure 4). In order to reach the final
spectroscopic orbital solution, we prepared a simple script written in Python
language, which applies Markov chain Monte Carlo simulations to the measured
radial velocities, considering their measured errors. We list the final
spectroscopic orbital elements in Table 2
and plot the measured radial velocities, their observational errors, the
theoretical spectroscopic orbit and residuals from the solution in Figure 2.
Fig. 2 (a) Observed radial velocities of the primary and the secondary
(blue and red filled circles, respectively), and their corresponding
theoretical representations (blue and red curve). (b) Residuals from
theoretical solution. The color figure can be viewed online.
3.2. Spectral Type
We rely on our intermediate resolution TFOSC optical spectra to determine the
spectral type of the components. Most of our spectra correspond to the phases
around orbital quadratures, where we observe the signal of the two components
separated. However, there are two spectra obtained at phases close to the
eclipses, where the two components can not be resolved separately. One of these
spectra corresponds to ≈ 0.56 orbital phase (see Table 1), where we cannot observe the radial velocity signal of the
secondary component in cross-correlation. Even at the orbital quadratures, the
cross-correlation signal of the secondary component is considerably weak
compared to the primary component, indicating a very small light contribution
from the secondary component to the total light of the system. Our preliminary
light curve analysis shows that the contribution of the secondary component to
the total light does not exceed ≈ 10%. In this case, the signal from the
secondary component becomes almost negligible at the resolution of our observed
spectrum at ≈ 0.56 orbital phase. Therefore, we assume that we only observe the
spectrum of the primary component and adopt this spectrum as reference spectrum
for the primary component. We confirm this assumption by calculating the
composite spectrum of the binary via final parameters of the components (see §
3.3), where we observe that the contribution of the secondary component affects
the theoretical composite spectrum less than 2% for the wavelength range of
4900-5700 ̊A. We refrain from performing a detailed analysis with spectral
disentangling. Future studies could take advantage of this technique and derive
atmospheric parameters of the secondary.
We first compare the reference spectrum with the template spectra of HD 225239
and ι Psc. We observe that ιPsc spectrum provides a closer match to the
reference spectrum but also indicates earlier spectral type and slightly lower
metal abundances for the primary component. At that point, we switch to the
spectrum synthesizing method. We use the latest version of python framework
iSpec (Blanco-Cuaresma et al. 2014) which
enables practical and quick calculation of a synthetic spectrum with a given set
of atmospheric parameters via different radiative transfer codes. Among these
codes we adopt the SPECTRUM4
code (Gray & Corbally 1994), together
with ATLAS-9 (Castelli & Kurucz 2004)
model atmospheres and the actual line list from the third version of the Vienna
atomic line database (V ALD3, Ryabchikova et al.
2015).
Considering the spectral type of ι Psc, we synthesize spectra for effective
temperatures between 6000 K and 7000 K in steps of 250 K, and metallicity values
([Fe/H]) between −1.0 and 0.0 in steps of 0.5. For all synthetic spectra we fix
the gravity (log g) to 4.15, which we precisely calculate by light curve
modelling (see § 3.3). Since we do not have a high resolution spectrum, we fix
the microturbulence velocity to 2 kms-1. We convolve all calculated
spectra with a proper Gaussian line spread function in order to degrade their
resolution to the resolution of the TFOSC spectra. Instrumental broadening in
TFOSC spectra is 2.2 ̊A, corresponding 119 km s-1 for wavelengths
around 5500 ̊A. The estimated projected rotational velocities of the components
are 62 km s-1 and 36 km s-1 for the primary and the
secondary component respectively (see § 3.3). Since instrumental broadening is
the most dominant broadening source in the observed spectra, we do not consider
rotational broadening and other line broadening mechanisms.
Among the calculated spectra we find that the model with 6500 K effective
temperature and an [Fe/H] value of −0.5 provides the closest match to the
reference spectrum. The final effective temperature indicates F5 spectral type
(Gray 2005). Considering the
effective temperature and metallicity steps in model atmospheres, and the
resolution of TFOSC spectra, the final values and their estimated uncertainties
are Teff = 6500±200 K and [Fe/H] = −0.5±0.5 dex, respectively. Note
that even if we considered the neglected contribution of the secondary component
in the reference spectrum, its effect would be within the estimated
uncertainties above. The final Teff value is ≈ 670 K lower than the
7166 K value estimated in Armstrong et al.
(2014). In Figure 3 we show
portions of the reference spectrum and the model spectrum, calculated with the
final parameters above.
Fig. 3 Representation of the observed (black), best matched (red)
synthetic spectrum and residuals (blue) for three regions. Note that
we shift the residuals upwards by 0.3 for the sake of
simplicity.
3.3. Light Curve Modelling and Physical Properties
Global visual inspection of KIC 9451096 Kepler photometry
reflects properties of a typical close eclipsing binary. We start the light
curve modelling by phasing the whole long cadence data with respect to the
ephemeris and period given by Borkovits et al.
(2016), and re-binning the phased data with a phase step of 0.002 via
the freely the available fortran code lcbin5 written by John Southworth. We plot the binned and
phased light curves of the system in Figure
4, panels a and aa. The light curve indicates a detached
configuration for the system. Mid-eclipse phases are 0.0 and 0.5 phases,
indicating a circular orbit. There is no conspicuous asymmetry in the light
curve.
Fig. 4 (a) Phase binned light curve of KIC9451096 (black filled circles)
together with best-fitting model (red curves). (b) Close up view of
the light curve at light maxima. c) Residuals from the best-fitting
model. Panels at right (aa, bb and cc) are the same as left panels
but for phased long cadence data. The color figure can be viewed
online.
We model the light curve with the 2015 version of the Wilson-Devinney code (Wilson & Devinney 1971; Wilson & Van Hamme 2014). In the
modelling, we first fix the most critical two parameters of the light curve
modelling, i.e., the mass ratio (q) of the system and the effective temperature
of the primary component (T1). Since we have reliably derived these
parameters in previous sections as q = 0.55 and T1 = 6500 K, we adopt
them as fixed parameters. The calculated atmospheric properties of the primary
component reveal that both stars have convective envelopes. Therefore, we set
albedo (A1 , A2 ) and gravity darkening (g1,
g2) coefficients of the components to 0.5 and 0.32, respectively,
which are typical values for stars with convective outer envelopes. We also
consider a slight metal deficiency of the system, and thus adopt the internal
stellar atmosphere formulation of the Wilson-Devinney code according to the
determined [Fe/H] value of −0.5. We assume that the rotation of the components
is synchronous with the orbital motion, and thus fix the rotation parameter of
each component (F1 , F2 ) to 1.0. We adopt a square root
law (Klinglesmith & Sobieski 1970)
for limb darkening of each component; this is more appropriate for stars cooler
than 9000 K. We take the limb darkening coefficients for the
Kepler passband (x1, x2,
y1, y2) and the bolometric coefficients
(x1bol , x2bol , y1bol , y2bol )
from van Hamme (1993). In the modelling,
we adjust inclination of the orbit (i), temperature of the secondary component
(T2), dimensionless omega potentials of the components (Ω1, Ω2)
and luminosity of the primary component (L1). We also include a phase
shift parameter as adjustable in the modelling, since we expect a shift in the
ephemeris due to the light-time effect of the third body (Borkovits et al. 2016). The model quickly converged to a
steady solution in a few iterations. We list the model output in Table 3 and we plot the best-fitting model
in Figure 4, panels a, b, and the residuals
from the model in panel c.
Table 3 Light curve modelling results of KIC9451096.a a (r1),(r2) denote the mean fractional radii of the primary and the
secondary components, respectively. Internal errors of the
adjusted parameters are given in parentheses for the last
digits. Asterisk symbols in the table denote fixed values for
the corresponding parameter. Note that we adopt the uncertainty
of T1 for T2 as well, since the internal error of T2 is
unrealistically small (∼1 K).
Parameter
Value
q
0.55*
T1(K)
6500*
g1, g2
0.32*, 0.32*
A1, A2
0.5*, 0.5*
F1 = F2
1.0*
phase shift
0.00108(2)
i (◦)
79.07(4)
T2(K)
5044(200)
Ω1
4.4942(49)
Ω2
4.8885(125)
L1/(L1+L2)
0.897(1)
x1bol, x2bol
0.136*, 0.293*
y1bol, y2bol
0.583*, 0.401*
x1, x2
0.106*, 0.482*
y1, y2
0.670*, 0.313*
(r1),(r2)
0.2557(3), 0.1506(5)
Model rms
3.0 × 10−4
In Figure 4, panel b, one can easily see the
model inconsistency around 0.25 orbital phase. The inconsistency indicates an
additional light variation, which is known as O´Connell effect, i.e. difference
between light levels of subsequent maxima in an orbital cycle. Possible sources
of the difference may be Doppler beaming, a hot spot or a cool spot on one of
the component of the system. KIC9451096 is a detached eclipsing binary, thus we
can safely exclude possibility of mass transfer between components, i.e., a hot
spot possibility. Doppler beaming was detected observationally among some
Kepler binaries (see, e.g. van Kerkwijk et al. 2010), which becomes important for systems with
very low mass ratios, especially for systems with a compact component, such as a
white dwarf or a hot sub-dwarf. In addition, if the effect is in progress, then
it would change the light levels of each maxima. However, we observe
inconsistency only for phase 0.25, while the model fairly represents the light
level at phase 0.75. Thus, Doppler beaming should have a negligible effect in
the case of KIC 9451096, if any. A remaining possibility is cool spots located
preferably on the cooler component.
Here we do not chose to model this inconsistency alone, which would only show the
cumulative effect of hundreds of light curves, but instead we subtract the
best-fitting model from the whole long cadence data and inspect the residuals in
order to investigate further light variations. We will focus on this in § 3.4.
We complete the light curve modelling section with a calculation of the absolute
parameters of the system by combining the spectroscopic orbital solution and
light curve model results. In Table 4, we
give the physical properties of each component. Our analysis reveals that the
system is formed by an F5V primary and a K2V secondary component.
Table 4 Absolute physical properties of KIC9451096.* *The error of each parameter is given in parantheses for the last
digits.
Parameter
Primary
Secondary
Spectral Type
F5V
K2V
[Fe/H]
−0.5 ± 0.5
Mass (M⊙)
1.18(26)
0.65(9)
Radius (R⊙)
1.53(10)
0.90(6)
Log L/L⊙
0.574(76)
−0.327(88)
log g (cgs)
4.14(4)
4.34(1)
Mbol (mag)
3.31(19)
5.57(22)
3.4. The Out-of-Eclipse Variations
In this section, we subtract the best-fitting light curve model from the whole
long cadence data and obtain residuals. Here, we first divide the whole long
cadence data into subsets, where each subset covers only a single orbital cycle,
resulting in 1026 individual light curves. Then we apply the differential
corrections routine of the Wilson-Devinney code and fix all parameters, except
the ephemeris reference time. In this way, we find a precise ephemeris reference
time for each individual subset, therefore eliminating any shift in the
ephemeris time due to the third body reported by Borkovits et al. (2016), and obtain precise residuals. In Figure 5, we plot three different parts of
the residuals. Note that we remove data points that correspond to the eclipse
phases due to the insufficient representation of the model at those phases. This
mainly arises from the inadequacy of radiative physics used in light curve
modelling for a very high photometric precision and can clearly be seen in Figure 4 panel c.
Fig. 5 (a) Residuals from whole long cadence data. Remaining panels show
different time ranges of residuals, where we observe different light
curve shapes, and flares.
Inspecting residual brightness, we immediately see a variation pattern which
changes its shape from time to time. Furthermore, we observe a sudden increase
and gradual decrease in the residual brightness which occasionally occurs over
four years of time span and has short time scale of a few hours. These patterns
are traces of magnetic spot activity, which is very possible for the K2V
secondary component. Observational confirmation of this possibility can be done
by inspecting magnetic activity sensitive spectral lines, such as the Hα and Ca
II H & K lines. We inspected these lines in our TFOSC spectra and did not
notice any emission features, which could be considered as the sign of the
activity. However, one should consider that the contribution of the secondary
component to the total light does not exceed 10% at optical wavelengths and will
steeply decrease towards the ultraviolet region of the spectrum. Furthermore,
the variation patterns observed in Figure 5
exhibit very small amplitudes. Therefore, the existence of magnetic spot
activity cannot be confirmed or excluded via spectral line inspection in the
case of KIC 9451096. Nevertheless, variation patterns and flares observed in the
residuals indicate weak magnetic spot activity in the secondary component, which
can still be detected with the very high precision of the
Kepler photometry.
We analyze rotational modulation and flares of the secondary component via
residuals by assuming that the source of all variation patterns is only the
secondary component.
3.4.1. Photometric Period and Differential Rotation
Conventional periodogram methods for determining rotational period do not
perfectly work in our case because the observed variation patterns exhibit quick
changes in amplitude and mean brightness level over short time scales of a few
days, which is comparable to the orbital period. Moreover, since we remove data
points at eclipse phases, this causes regular gaps in the data which repeat each
≈ 0.625 day (i.e. half of the orbital period); thus, it causes an alias period
and its harmonics, and disturbs the real periods. Furthermore, one can clearly
see that the rotational modulation of residuals has an asymmetric shape.
Considering an individual light curve with an asymmetric shape, it is not
possible to find a single period to represent the whole light curve perfectly,
and additional periods (i.e. harmonics) are required. Therefore we apply an
alternative method based on tracing the time of a minimum light observed in an
orbital cycle, which was previously applied to RS CVn system HD 208472 (özdarcan et al. 2010). For each orbital
cycle, we find the time of the deepest minimum in the cycle by fitting a second
or third order polynomial to the data points around the expected minimum time.
The order of the polyno Subset mial depends on the light curve shape. After
obtaining all minimum times, we construct an O − C diagram by adopting the first
minimum time observed in the residuals as initial ephemeris reference time, and
the orbital period as the initial period, and obtain O−CI values. Then we apply
a linear fit to the O−CI values and calculate an average ephemeris reference
time and period given in Equation 1, together 6 with statistical uncertainties
given in parentheses for the last digits.
(1)
In the equation, T0(BJD) and E denote ephemeris reference time and
integer cycle number, respectively. We plot O − CI values and linear fit in
Figure 6, panel a. After obtaining an
average ephemeris and period, we subtract the linear fit from O−CI data and
obtain O−CII data, which in principle shows the real period variation for a
given time range. Figure 6, panel b shows O
− CII data. We divide O − CII data into 30 subsets by grouping data points that
appear with a linear slope. The linear trend of a subset gives the difference
between the best-fitting photometric period of the subset and the grand average
photometric period given in Equation 1. Therefore we can calculate a mean
photometric period for each subset. We plot the calculated mean photometric
periods versus time in Figure 6, panel c,
together with the statistical uncertainties. We list photometric periods for 30
subsets in Table 5, and tabulate our O −
C analysis results in Table 8.
Fig. 6 (a) O−CI diagram of observed minimum times (blue filled circles)
and linear fit (red line).
Table 5 photometric periods found from O − C analysis
Subset
BJD (24 00000+)
P (day)
σ(P) (day)
1
54994.8107
1.2456
0.0004
2
55048.8731
1.2326
0.0008
3
55094.1598
1.2441
0.0004
4
55139.0644
1.2260
0.0019
5
55169.9192
1.2459
0.0008
6
55208.0721
1.2489
0.0006
7
55250.0831
1.2584
0.0011
8
55314.8252
1.2484
0.0004
9
55366.4562
1.2355
0.0006
10
55425.0957
1.2470
0.0006
11
55478.0779
1.2517
0.0010
12
55507.4240
1.2437
0.0006
13
55539.3828
1.2216
0.0025
14
55629.1787
1.2430
0.0004
15
55702.5236
1.2447
0.0004
16
55740.2684
1.2522
0.0007
17
55793.0150
1.2485
0.0004
18
55840.9410
1.2223
0.0022
19
55868.2947
1.2534
0.0005
20
55894.6874
1.2712
0.0022
21
55924.7567
1.2494
0.0006
22
55960.4676
1.2391
0.0011
23
55996.8636
1.2507
0.0005
24
56026.2172
1.2474
0.0009
25
56073.0738
1.2528
0.0005
26
56136.3924
1.2449
0.0005
27
56258.6328
1.2509
0.0004
28
56333.3104
1.2323
0.0019
29
56359.5423
1.2565
0.0008
30
56400.8932
1.2504
0.0004
The average period given in Equation 1 represents the average rotation period for
magnetic activity features on the surface of the secondary component, which are
typically cool and dark regions, i.e., star spots, and indicates a slightly
(∼0.5% day) shorter period compared to the orbital period. This is clearly
observed in Figure 6 panel c, where the
mean photometric periods of subsets are mostly shorter than the orbital period.
Assuming a solar type differential rotation, this means that the orbital period
is slightly longer than the equatorial rotation period of the secondary
component. Under the same assumption, the differential rotation coefficient can
be estimated from (Pmax −Pmin)/Pequ = kf, where
Pmax , Pmin , k and f denote observed maximum and
minimum period, differential rotation coefficient and a constant that depends on
the range of spot forming latitudes, respectively (Hall & Busby 1990). Considering the small amplitude of
rotational modulation of residuals, we assume that the secondary component is
not largely spotted and that the total latitudinal range of the spot
distribution is 45 degrees, which causes the f constant to take values between
0.5 and 0.7 (Hall & Busby 1990).
Using maximum and minimum photometric periods from the O − C analysis, and
assuming that the shortest period corresponds to the equatorial rotation period
of the star, we find k = 0.081 ± 0.011 and k = 0.058 ± 0.006 for f = 0.5 and f =
0.7, respectively. Since these k values are calculated via boundary values of f,
the real differential rotation coefficient must lie in the range of k values
calculated above. An average k is found as 0.069±0.008.
3.4.2. Flares
We detect 13 flares in the residuals from long cadence data. In the flare
analysis, it is critical to determine the quiescent level, which denotes the
brightness level in the absence of a flare. In our case, we determine the
quiescent level by applying Fourier analysis to the single orbital cycle where
the flare occurs. The Fourier analysis represents the rotational modulation of
residuals in the cycle, and then we remove the Fourier representation from the
data. The remaining residuals show only the quiescent level and the flare
itself. We show such a flare light curve in Figure
7.
Fig. 7 An example of a flare light curve. The filled black circles
represent the observations, while the red line represents the
quiescent level derived from the data out-of-flare. The color figure
can be viewed online.
The energy (E) is a very important parameter for a flare. However, the energy
parameter has the luminosity L of the star as a factor in equation E = P × L
described by Gershberg (1972). Due to the
disadvantages described in Dal & Evren
(2010), we use the flare equivalent duration instead of the flare
energy, which is more proper. We compute the equivalent durations of flares via
the equation P = [(Iflare − I0)/I0]dt (Gershberg 1972), where P is the flare
equivalent duration in seconds, I0 is the quiescent level intensity,
and Iflare is the intensity observed at the moment of the flare. Considering the
quiescent level, the times of flare beginning, flare maximum and flare end are
determined, together with flare rise duration, flare decay duration and flare
amplitude. We list all computed values in Table
6 for each of the 13 flares.
Table 6 The parameters calculated for each
BJD (24 00000+) 55021.2171
P (s) 11.4
Tr (s) 1763
Td (s) 15889
Amp (mag) -0.001516
55043.1016
5.6
1763
5296
-0.002483
55310.6569
7.6
1763
8830
-0.002047
55326.5140
2.7
1771
1763
-0.001618
55412.0302
5.9
1763
7068
-0.001648
55416.9343
12.1
1771
14118
-0.002853
55824.2162
4.3
1763
5296
-0.001578
55931.1213
4.5
3534
3534
-0.001453
55971.7021
4.9
1763
5296
-0.002152
56142.9809
6.0
3534
7059
-0.001983
56284.8887
3.4
1771
3525
-0.001806
56286.5642
4.4
1771
3525
-0.001568
56375.4705
2.2
1763
1763
-0.001429
Dal & Evren (2010, 2011) suggest that the best function to
represent the relation between flare equivalent duration and flare total
duration is the OPEA, where the flare equivalent duration is considered on a
logarithmic scale. The OPEA function is defined as y = y0
+(Plateau−y0)×(1−e−kx), where y is the flare equivalent duration on a
logarithmic scale, x is the flare total duration, and y0 is the flare equivalent
duration in the logarithmic scale for the least total duration, according to the
definition of Dal & Evren (2010). It
should be noted that the y0 does not depend only on the flare mechanism, but
also depends on the sensitivity of the optical system used in the mission. The
most important parameter in the model is the Plateau value, which defines the
upper limit for the flare equivalent duration on a logarithmic scale and is
defined as the saturation level for a star (Dal
& Evren 2011). Using the least squares method, the OPEA model
leads to the results in Table 7. We plot
the resulting model in Figure 8 with its
95% statistical sensitivity limit.
Table 7 Parameters derived from the OPEA *Using the least squares method.
Parameter
Value
Y0
−0.015961±0.13891
Plateau
1.2394±0.14441
K
0.00011438±0.000036715
Half-time
6060
R2
0.94535
P value
∼0.10
Fig. 8 The OPEA model obtained over 13 flares. The blue filled circles
show each flare while the continuous red line shows the OPEA model
and the dotted red lines show the sensitivity range of the model.
The color figure can be viewed online.
We tested the derived model by using method proposed by D’Agostino & Stephens (1986) to understand whether there
are any other functions to model the distribution of flare equivalent durations
on this plane. In this method, the probability value (P value), is found to be ≈
0.10, which means that there is no other function to model the distributions
(Motulsky 2007; Spanier & Oldham 1987).
Ishida et al. (1991) described a
frequency for the stellar flare activity as N1 = Σnf
/ΣTt, where Σnf is the total flare number detected in
the observations, while ΣTt is the total observing duration from the
beginning of the observing season to the end. In the case of KIC9451096 we find
the N1 frequency as 0.000368411 h-1 adopting the total
long cadence observing duration as 1470.2786 days from the times of the first
and last long cadence data points.
4. Summary and discussion
Photometric and spectroscopic analysis of KIC9451096 reveals that the system is
composed of an F5V primary and a K2V secondary star in a circular orbit with a
detached binary configuration. Medium resolution TFOSC spectra suggest that the
system has one third of the [Fe/H] of the Sun. Light curve modelling reasonably
represents the observations. However, we are able to catch the signals of additional
light variation, which is very weak compared to the variations due to the binarity
and eclipses, but still observable due to the very high precision of the
Kepler photometry.
We observe occasional flares and rotational modulation of the light curve residuals
from the eclipsing binary model. Considering the physical and atmospheric properties
of the components, we attribute these variations to the secondary component, which
is a perfect candidate for magnetic star spot activity with its deep convective zone
owing to its spectral type and very fast rotation caused by short orbital period. We
inspect rotational modulations of the residuals to trace the photometric period of
the secondary component, and analyze its flare characteristics.
Photometric period analysis via O − C diagrams shows that the average photometric
period is shorter than the orbital period by ≈ 0.5% day. Under any type of
differential rotation assumption (either solar like, or anti-solar like), this means
that the orbital period does not correspond to the equatorial rotation period of the
star. Following the method proposed by Hall &
Busby (1990), we find an average differential rotation coefficient of k =
0.069 ± 0.008, suggesting ≈ 3 times weaker differential rotation compared to the
solar value of 0.19. We note that the type of differential rotation cannot be
determined from photometry alone and we implicitly assume a solar type differential
rotation in the case of KIC 9451096. However, the k = 0.069 value, which is
extracted from very high precision continuous photometry for a restricted time range
(four years in our case), defines a lower limit for the strength of the differential
rotation of the star. A quick comparison of k values for other stars can be done by
looking at the 17 stars listed in Hall & Busby
(1990), where k values are usually a few percent or less, except for BY
Dra with k = 0.17.
A more reliable way of detecting differential rotation with its magnitude and type is
Doppler imaging, which is based on high resolution time series spectroscopy.
Considering other stars whose k values were determined by Doppler imaging, we see
mostly weak differential rotation with a k value of a few percent, both among solar
type differential rotators (HD 208472 k = 0.015 (özdarcan et al. 2016), XXTri k = 0.016 (Künstler et al. 2015), ζ And k = 0.055 (Kövári et al. 2012), KUPeg k = 0.04 (Kövári et al. 2016)) and among anti-solar type differential rotators
(UZLib k = −0.004 (Vida et al. 2007), σ Gem k
= −0.04 (Kövári et al. 2015), HU Vir k =
−0.029 (Harutyunyan et al. 2016)). Due to the
binary nature of KIC 9451096, a considerable effect of tidal forces on the
redistribution of the angular momentum in the convective envelope of the components
can be expected, which would alter the magnitude of differential rotation (Scharlemann 1982). Based on observational
findings, Collier Cameron (2007) suggests
suppression of differential rotation by tidal locking, which is possibly in progress
for KIC 9451096.
We detect 13 flares in the residuals from long cadence data, which are attributed to
the secondary component with a corresponding B − V value of 0m.92 (Gray 2005). We apply the OPEA model to analyze
flare characteristic and find that the calculated flare parameters and resulting
OPEA model parameters seem to be in agreement with parameters derived from stars
analogous to the secondary component, except for the half-time value. A possible
source of disagreement for the half-time value is that there are not enough sample
flares at the beginning of the OPEA model.
We find an N1 value of 0.000368411 h-1 for KIC9451096. N1 was
found to be 0.41632 h-1 for KIC09641031 (Yolda ̧s & Dal 2016), 0.01351 h-1 for KIC 09761199 (Yolda ̧s & Dal 2017), and 0.02726
h-1 for Group 1 and 0.01977 h-1 for Group 2 of KIC 2557430
(Kamil & Dal 2017). Among these
systems, KIC9451096 has the lowest N1 value, which indicates that the
magnetic activity level of the secondary component of KIC 9451096 is the lowest,
according to Dal & Evren (2011).
We thank TüBI ̇TAK for partial support in using RTT150 (Russian-Turkish 1.5-m
telescope in Antalya) with project number 14BRTT150-667. This paper includes data
collected by the Kepler mission. Funding for the
Kepler mission is provided by the NASA Science Mission
Directorate.
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Appendix
A.1. O − C analysis results
We tabulate O − C analysis results in Table 8. N is the number of the minimum,
beginning from the first observed minimum in the data set. E is the decimal
cycle number and E rounded is the rounded E number to the nearest integer or
half integer. Note that as time progress O − C differences approach a cycle.
When this the occurs, one needs to add an additional increment of 0.5 to the E
rounded value in order to see O − CI diagram on a trend without any
discontinuity.
H. A. Dal, O. Özdarcan, and E. Yoldaş: Ege University, Science Faculty, Department of Astronomy and Space Sciences,
35100 Bornova, Izmir, Turkey (orkun.ozdarcan@ege.edu.tr).
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