A&A 469, 339-346 (2007)
DOI: 10.1051/0004-6361:20077175
B. Vrsnak - D. Sudar - D. Ruzdjak - T. Zic
Hvar Observatory, Faculty of Geodesy, Kaciceva 26, 10000 Zagreb, Croatia
Received 26 January 2007 / Accepted 16 March 2007
Abstract
Context. Basic observational parameters of a coronal mass ejection (CME) are its speed and angular width. Measurements of the CME speed and angular width are severely influenced by projection effects.
Aims. The goal of this paper is to investigate a statistical relationship between the plane-of-sky speeds of CMEs and the direction of their propagation, hopefully providing an estimate of the true speeds of CMEs.
Methods. We analyze the correlation between the plane-of-sky velocity and the position of the CME source region, employing several non-halo CME samples. The samples are formed applying various restrictions to avoid crosstalk of relevant parameters. For example, we select only CMEs observed to radial distances larger than 10 solar radii; we omit CMEs showing a considerable acceleration in the considered distance range and treat CMEs of different angular widths separately. Finally, we combine these restriction criteria, up to the limits beyond which the statistical significance of the results becomes ambiguous.
Results. A distinct anti-correlation is found between the angular width of CMEs and their source-region position, clearly showing an increasing trend towards the disc center. Similarly, all of the considered subsamples show a correlation between the CME projected speed and the distance of the source region from the disc center. On average, velocities of non-halo limb-CMEs are 1.5-2 times higher than in the case of non-halo CMEs launched from regions located close to the disc center.
Conclusions. Unfortunately, the established empirical relationships provide only a rough estimate of the velocity correction as a function of the source-region location. To a certain degree, the results can be explained in terms of CME cone models, but only after taking crosstalk of various parameters and observational artifacts into account.
Key words: Sun: coronal mass ejection (CMEs)
Observations of coronal mass ejections (CMEs) are strongly affected by projection effects (e.g., Burkepile et al. 2004; Schwenn et al. 2005, and references therein). Since single-coronagraph observations provide only the plane-of-sky measurements of the CME postion, the true radial distances, velocities, accelerations, and angular widths are generally not known. Exceptionally, the true velocity and acceleration can be derived when spectrographic measurements are available (e.g., Raymond et al. 2003; Ciavarella et al. 2005, and references therein).
Understanding of projection effects is important for two reasons. Since the observed kinematics, geometry,
and morphology of an eruption is severely influenced by the perspective effects, they also place an important
limitation on our understanding of physical characteristics of CMEs. Secondly, the projection effects play an
important role in the context of the space weather predictions (e.g., Michaek et al. 2003;
Burkepile 2004; Xie et al. 2004; Schwenn et al. 2005; Xue et al. 2005; and references therein).
The relationship between the measured and the true height, velocity, and acceleration of a CME depends on the position of the source-region, the shape of the CME, and the offset of the CME motion from the radial direction. There were several attempts to model projection effects by assuming various geometrical forms of CMEs (e.g., Hundhausen et al. 1994; Sheeley et al. 1999; Leblanc et al. 2001; Zhao et al. 2002; Thernisien et al. 2006). However, due to the unknown 3-dimensional morphology of a CME, the model-based corrections are quite ambiguous, especially if applied to case studies. Most often, it is presumed that CMEs move radially, and the cone shape is applied.
Generally, the model-based procedures employed to infer the true CME velocity could be divided into two classes. In the case of non-halo CMEs, when legs of a CME can be clearly identified, one may apply the model correction straightforwardly, just by measuring the kinematics of the farthest element of the CME leading edge (e.g., Goplaswamy et al. 2001; Yeh et al. 2005). On the other hand, in the case of halo and partial-halo CMEs, launched from regions located close to the disc center, the procedure includes measurements over the entire oval shape of the outer rim of the CME (e.g., Xie et al. 2004; Xue et al. 2005), or at least measurements of the two main axes of the ellipse (e.g., Schwenn et al. 2005).
Unfortunately, it turns out that applying the "correction'' usually results in an increase in the data scatter, especially in the case of the former procedure (non-halo CMEs). The correlations between various parameters found from raw data get degraded or even smeared out after applying the correction (e.g., Goplaswamy et al. 2001; Moon et al. 2002; Yeh et al. 2005). Probably, the problem lies in the mentioned model-based methods relying on a prescribed geometrical shape of CMEs, whereas the CME shapes depend on a number of factors and most likely differ significantly from one event to another (e.g., Cremades & Bothmer 2004).
Therefore, in this paper we study projection effects from the empirical point of view. In particular, we
analyze the statistical relationship between the mean CME velocity
and the plane-of-sky distance
of the CME source region from the disc center. We employ a large CME sample to compare
measured at
different
,
with speeds of CMEs launched from the close-to-limb regions. Supposing that the latter are
not affected by the projection effects, a correction factor may be derived, providing an estimate of the true
CME velocity.
In Sect. 2 we present the data set and basic characteristics of the CME samples used in the analysis, to get
insight into the crosstalk of different parameters that could affect the results. In Sect. 3 we analyze the
relationship employing different susbsets of CMEs in trying to avoid the effects of these
crosstalks. In Sect. 4 we discuss the outcome in the frame of three CME cone-model options that are specified
in the Appendix. Finally, we consider implications of the results and discuss limitations of possible
applications.
The following analysis employs a sample of CMEs observed in the range 2-30 solar radii by the Large Angle and Spectrometric COronagraph (LASCO; Brueckner et al. 1995) in the period 1996-2005. We utilize measurements compiled in the online LASCO CME Catalog (http://cdaw.gsfc.nasa.gov/CME_list/; Yashiro et al. 2004). Since the information on the CME source region is needed for the analysis of projection effects, the CME sample was complemented by the data concerning soft X-ray (SXR) flares, for which positional information is available (ftp://ftp.ngdc.noaa.gov/STP/SOLAR_DATA/SOLAR_FLARES/XRAY_FLARES/).
In associating flares with CMEs we used spatial and temporal criteria described in Vrsnak et al. (2005). In the analysis we considered only CMEs whose leading-edge position was measured in at
least four instances. For each CME that satisfied this requirement, we used the linear back-extrapolation of
its trajectory to the surface of the Sun in order to estimate the "take-off time'' t0. Then, following the
statistical procedure proposed by Dougherty et al. (2002), we inferred that the flares that
occurred out of the temporal window
days are most likely not associated with a given CME
(0.04 days
1 h). In this way we established a set of CME-flare pairs whose relative timing
was indicative of a causal relationship. In the next step we required the position angle of the flare to lie
within the position angle interval spanned by the CME. Finally, we excluded all cases where more than one
flare was satisfying the described temporal and spatial criterion, as well as the cases where one flare could
be attributed to more than one CME.
In this way we established a sample of 1145 flare-CME pairs (hereinafter denoted as the f-sample), for which it can be presumed that the flare was an intrinsic part of the CME process (e.g., Forbes 2000). For these events, we identify the position of the CME source region with the flare position. In the previous study (Vrsnak et al. 2005), it was shown that the described matching procedure results in a certain fraction of wrong CME-flare identifications (about 6% turned out to be back-side CMEs), which however does not affect the statistical results significantly.
In addition, as a "control'' sample, we used a set of 211 CMEs associated with disappearing solar filaments
(DSF) and eruptive prominences at the limb (EPL) as reported in Solar Geophysical Data in the period
1996-2001. Hereinafter, we call this the p-sample. A part of this sample (104 events), containing only
DSF-associated CMEs that were launched from ,
was used by Vrsnak et al. (2005).
The CME kinematical parameters are determined from measurements of the plane-of-sky heliocentric distances of
the leading edge of CMEs, R(t), expressed in units of the solar radius,
.
We employed the
following parameters available in the LASCO CME Catalog:
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Figure 1: Relationship between various parameters in the complete f-sample: a) mean velocity and angular width; b) mean velocity and largest measured distance; c) angular width and the distance of the source region from the disc center; d) mean velocity and the 1-8 Å peak flux of the associated SXR flare. Black circles represent halo-CMEs. Linear least-square fit parameters are given in the insets (black - complete sample, gray - non-halo CMEs, C is the correlation coefficient). The statistical significance of all correlations is greater than 99.99%. |
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In Fig. 1 we show several basic characteristics of the employed sample that are relevant for the
following analysis and the interpretation of results. In Fig. 1a the correlation between the CME mean
velocity
and the angular width W is presented. We find a distinct correlation, showing that wider
CMEs are on average faster (for a similar relationship see, e.g., Hundhausen et al. 1994; Yashiro et al. 2004; Vrsnak et al. 2004, 2005). Average values are
and
km s-1. If halo CMEs are excluded, we find
and
km s-1.
Figure 1b shows the correlation between the radial distance up to which a CME was traced, ,
and
the CME velocity. On average, faster CMEs can be traced to greater heights. The distribution of data points
also illustrates that halo CMEs tend to be faster than non-halo CMEs (check also Fig. 1a).
The dependence of angular width on the source-region position is presented in Fig. 1c. The correlation
reveals that CMEs launched from locations closer to the disc center tend to have larger angular widths, as
expected from the CME cone-model (e.g., Yeh et al. 2005). It should be also noted that there is a
considerable number of data points representing halo CMEs close to the limb (
at
). It is quite likely that at least some of these events were back-side CMEs, erroneously associated with
some limb flares (note that spatial criterion defined in Sect. 2 is meaningless in the case of halo CMEs).
In Fig. 1d we show the relationship between the CME velocity and the SXR importance (peak flux) of the associated flare. The correlation shows that CMEs associated with stronger flares are on average faster (see also, e.g., Moon et al. 2002; Burkepile et al. 2004; Vrsnak et al. 2005).
The CME data do not show any correlation between the farthest distance
and
,
or between the
acceleration a and
.
Correlations very similar to that shown in Figs. 1a-d are also found
for the p-sample.
The complete sample of 1145 CMEs does not show any correlation between the position
and the CME
velocity
,
as would be expected considering projection effects (see Appendix). In this section we
analyze the
relationship in more detail, employing several subsamples that were formed by
successively applying more restrictive conditions to those CME parameters that presumably might affect the
outcome. For example, first we exclude halo CMEs. We focus on non-halo CMEs for two reasons: i) the
chance of an erroneous flare-CME association is greater than in normal CMEs (the spatial criterion is
ill defined); ii) halo CMEs propagate along the line-of-sight so we observe the expansion velocity
rather than the radial one. The latter effect requires a completely different approach to the problem (e.g.,
Zhao et al. 2002; Micha
ek et al. 2003; Xie et al. 2004; Xue et al. 2005; Schwenn et al. 2005, and references therein).
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Figure 2:
a) CME mean velocities ![]() ![]() ![]() |
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In Fig. 2a we show the correlation
for the complete non-halo f-sample by including only
the events with
.
Although the correlation is weak (small correlation coefficients C), it
has a high statistical significance of P>99.98%; i.e., the correlation is certainly not accidental, since
the significance of P> 99.98% means that the probability of a random distribution of data points (i.e.,
no correlation) is lower than 0.02%.
The large scatter (and thus the low correlation coefficient) is a direct consequence of the broad range of
true CME velocities. Considering only CMEs that occurred close to the solar limb, we find that true
velocities range from 100 to more than 1500 km s-1. Checking the velocity range by moving towards the
disc center, we see that the
range decreases to approximately 100-1000 km s-1 at low values
of
.
This trend is roughly outlined in Fig. 2a.
It is also important to note that the lower limit of
values in Fig. 2a remains around 100 km s-1 over the whole
range. This is most likely an observational artifact; i.e.,
the events with
km s-1 are rarely reported as CMEs. Another possible reason is that
low-velocity CMEs that are launched from regions located close to the disc center, need a long time/distance
before they appear above the coronagraph occulting disc, and quite likely fade out before that. The effect of
a constant lower limit over the whole
range decreases the slope of the regression line and further
reduces the correlation coefficient.
To estimate how much the broad range of velocities and the constant lower limit influence the correlation, we
prepared an artificial sample of CMEs, consisting of 15 CME subsets characterized by the true velocities
v*=100, 200, 300, ..., 1500 km s-1, each containing 6 CMEs launched from ,
0.2, 0.4, 0.6,
0.8, and 1. Furthermore, we considered that the observed velocities behave as
,
where we took
k=500 km s-1. Note that v0=v*-k, since v*=v at
.
After joining all subsets and
applying the lower limit of observed velocities to 100 km s-1, the correlation coefficient decreased to
(for a subset of given v* it amounts to C=1), whereas the slope became around two times
flatter than the original slope k.
Taking the linear least-square fit parameters from Fig. 2a, one finds that CMEs launched from the
close vicinity of the solar disc center are on average slower by a factor
than those
launched from the limb regions. We can compare this value with the values derived from the three cone-model
options described in the Appendix. The sample shown in Fig. 2a is characterized by the average angular
width of
,
and for such a width the cone models A, B, and C described in the
Appendix, give values
,
2, and 2.5, respectively. Whereas the model A value might be
considered as comparable to the observed one, the values based on models B and C are considerably higher.
Even taking into account the decreased slope of the correlation due to the previously mentioned effects, one
finds the ratio
is not higher than
1.7.
On the other hand, focusing on the thin or dashed line in Fig. 2a, which roughly outline the
decreasing trend of the range towards the disc center (hereinafter "upper limit'' trend), we find a
considerably higher values of
,
ranging between 2 and 3. Such values are roughly in the range
expected for the cone models B and C.
To define the decreasing trend in the
range in a more quantitative way, we present the 2-dimensional
distribution in Fig. 2b of the data-points from Fig. 2a. The first isoline shows a trend from
some 1000-1200 km s-1 at
down to about 500 km s-1 at
.
This corresponds to
the ratio
;
i.e., very close to the values derived from the cone models B and C.
In Fig. 2c we display the
correlation for the complete non-halo p-sample. Utilizing the
linear least-square fit parameters, we find
.
The mean angular width of CMEs in the
non-halo p-sample equals to
,
and for such a width models A, B, and C give
,
2.0, and 2.4, respectively. The model B and C values are close to the measured ones,
whereas model A gives considerably lower values. Again, we outline the decreasing trend of the
range.
The values of
based on these lines are found to be around 3; i.e., somewhat higher than the
model values.
Table 1:
Characteristics of the correlation
,
specified for the
non-halo CME samples displayed in Figs. 2-4. The values
,
,
and
displayed in the last column
represent the values of
derived from models A, B, and C, respectively.
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Figure 3:
The correlation between mean velocities and the source-region position for:
a) non-halo f-sample restricted to
![]() ![]() ![]() |
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Bearing in mind the relationships presented in Fig. 1 and the corresponding crosstalk of parameters,
we reduce our f-sample by excluding events with
.
Furthermore, to exclude the effects of
acceleration, we consider only events with
m s-2: events launched at small
are observed in the late phase of the eruption, when the main acceleration is over, whereas a significant
part of CMEs still accelerates in the case of limb events (e.g., Feynman & Ruzmaikin 2004; Vrsnak
et al. 2005). Finally, we subdivide the sample into W-bins, since it is expected that the
projection effects depend on the CME geometry (see Appendix).
Successively applying a more restrictive acceleration limit; i.e., decreasing the limiting value from, e.g.,
to
m s-2, we found that the slope of the
relationship
is systematically increasing. A similar effect we find also if we successively increase the limiting value of
.
In Fig. 3a we show the non-halo f-sample, including only the events with
m s-2,
.
We see that the slope and the correlation coefficient are larger than in
Fig. 2a. Taking the parameters of the linear least-square fit, we find that the ratio of
at
and
amounts to
.
This value is relatively close to the values derived from
models A and B, adding up to 1.4 and 1.9. On the other hand, it is considerably lower than that obtained from
model C, amounting to 2.3. Considering the "upper limit'' trend,
ranges between 2 an 2.5. These
values are quite close to what is expected from cone models B and C, which give the ratios of 1.9 and 2.3,
respectively.
Analogously, in Fig. 3b we show the non-halo p-sample; however, since the p-sample is considerably
smaller, we could only take the less restrictive condition
m s-2 (instead of
m s-2). The linear least-square fit gives the value of
,
which is
considerably higher than the values based on models A, B, and C, which for
equal to 1.4, 2.0, and 2.4, respectively. Again, we indicate the "upper limit'' trend in Fig. 3b, from which we
find
ranging between 3 and 5. These values are much higher than the model values, but it should
be noted that the "upper limit'' lines in this case are based on quite a small number of data points
(especially the dotted one).
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Figure 4:
The correlation between mean velocities and the source-region position for the reduced non-halo CME samples
shown in Fig. 3, divided in W-bin subsamples:
a) f-sample (
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Since the projection effect on
is likely to be stronger for CMEs of smaller widths (see Appendix), we
subdivide the sample presented in Fig. 2a into three
W-bins:
,
,
(the bin
includes a small number of events, and the results are statistically insignificant).
The results are shown in Fig. 4a. Applying still more stringent conditions or narrowing W-bins
reduces the samples too much, so the correlations become statistically insignificant. The three considered
subsamples consist of N=89, 92, and 68 events. The mean widths are
,
,
and
.
Figure 4a shows that the bin
displays a steeper slope than
the last two, but the last two are very similar. The ratios
amount to 1.76, 1.42, and 1.45 for
the three subsets, respectively, and it should be noted that the differences are of low statistical
significance. The values for the two narrowest bins are considerably lower than the model values, whereas
for the widest bin is close to the model A value (compare the last two columns of Table 1
where we present the observed and the model-based values).
In Fig. 4b we show results for the p-sample taking only the CMEs with
m s-2and dividing them into
bins. The two considered subsamples consist of 41 and 50 events.
The mean widths are
and
.
The ratio
equals 4.10 and 1.37, respectively.
The former value is somewhat higher than the model values, whereas the latter one is comparable with the
model A value (see the last column of Table 1). The difference between the two subsets is within the
accuracy of the fit parameters; i.e., it again has low statistical significance.
Bearing Fig. 1d in mind, we also checked the correlations by employing only events associated with SXR C-class flares (the most abundant subset). It turned out that the outcome is more or less the same as when not applying the SXR-class restriction; i.e., differences are statistically insignificant.
Basic characteristics of the
correlations presented in Figs. 2-4 are
summarized in Table 1. After defining the samples in the first three columns, we display the number of
events in the sample N, and the mean angular width of CMEs in the sample,
.
In the next five
columns we present the slope k of the regression line, the y-axis intercept v0 of the regression line,
the statistical F-test significance of the correlation, the correlation coefficient C, and the ratio
of the
values at
and
.
In the last column we display the values of
derived from models A, B, and C, denoted as
,
,
and
,
respectively.
Bearing in mind the effects discussed in Sect. 3.1, the values of the factor
obtained from the
linear least-square parameters listed in Table 1 are most likely underestimated; i.e., the correction
factor is likely to be larger. Indeed, inspecting Table 1 we find that in most cases the value of
is lower than the model values.
The parameter
represents the empirical factor by which one should multiply the velocity of a CME launched from a close-to-center source region in order to get its true velocity. In fact, a correlation
between the CME velocities and the source-region position, expressed in the form
,
can be
utilized to obtain factor
,
by which the observed velocity v of a CME that was launched from
any position
should be multiplied to get its true velocity v*:
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(1) |
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Figure 5:
Comparison of the empirical and the model-based correction factors
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We summarize the results of the presented analysis as follows:
Although the presented analysis reveals a distinct correlation between the CME speed and position, from the
obtained results it is difficult to establish an unambiguous empirical relation to be used for deriving a
true CME speed from the measured one. The values of
based on the parameters of the linear
least-square fit for different subsamples, generally range from 1.5 and 2. However, the
trend for
the fastest events indicates that
may be higher by a factor of two; i.e., the correction based on
the least-square fit should be considered as a lower limit.
It is interesting to note that, although the cone model A should be considered as geometrically less
realistic, it shows a better agreement with our results based on the least-square fit procedure than models B
and C. On the other hand, models B and C show a better correspondence with the
behavior for the
fastest events ("upper limit'' trend). This again indicates that the correction factor based on the
least-square fit procedure is probably underestimated and that the "upper limit'' procedure gives more
appropriate values. Finally, it should be noted that the CME cone models predict a larger correction factor
for narrower CMEs. Although our results indicate such a trend, the differences have very low statistical
significance, and the results are not reliable enough to provide a clear
dependence.
In this respect, it should be noted that the CME cone model is a purely morphological geometric concept, not founded on physical considerations. Thus, it is instructive to compare our results with models that are based on the physics of the eruption. In particular, we pay attention to the geometry included in models, since it is the main factor when projection effects are considered. Unfortunately, this aspect is treated only occasionally and only in an illustrative way (e.g., Tokman & Bellan 2002; Thernisien et al. 2006; Krall et al. 2006), because most of the models are focused on the dynamics of the eruption.
According to the geometry, magnetohydrodynamical models of CMEs could be classified into "global'' models and "local'' ones. The first class treats the eruption as a global process, taking place in a large-scale coronal streamer. Consequently, the eruption is most often treated as a 2-dimensional (2-D) or 2.5-D process in the spherical geometry, where the pre-eruptive coronal streamer, either bipolar (e.g., Mikic & Linker 1994; Cargill & Schmidt 2002; Jackobs et al. 2006, and references therein) or quadrupolar (e.g., Antiochos et al. 1999), is sited on, or parallel to, the solar equator. Due to the axial symmetry involved, these models are not affected by the projection effects. Since our results show the dependence of the plane-of-sky velocity and the CME width on the source-region position, it can be concluded that situations where such 2-D and 2.5-D axially symmetric models could be applied are relatively rare (large-scale eruptions oriented in the East-West direction and occupying a very wide range of solar longitudes).
The most advanced global models, whose development has begun only recently, start from a realistic magnetohydrodynamical state of the corona and the solar wind, and the eruption only includes a limited magnetic structure in the corona (e.g., Fry et al. 2003; Manchester et al. 2004; Odstrcil et al. 2004; Odstrcil et al. 2005, and references therein). The model results reveal a wide variety of morphological patterns and evolutionary characteristics of eruptions. Unfortunately, the projection effects are never directly treated in this type of model. However, since only a fragment of the corona is included in the eruption, it is natural to expect that the outcome is affected by the projection effects; i.e., that the plane-of-sky velocity and the CME width depend on the source-region position. That can be seen directly from the presentation of model results that often includes various viewing angles to represent the results more transparently. This variety of morphological and evolutionary forms, probably leads to complex projection effects that are much more intricate than expected from the simple cone model.
In contrast to global models, which primarily treat the propagation of CMEs in a realistic ambience, "local''
models are focused on the processes causing the take-off and acceleration of the eruptive coronal structure.
Most of these models invoke magnetic structures that include semi-toroidal flux-rope embedded in the magnetic
arcade and anchored at both ends in the dense photosphere (for the development of the flux-rope concept see,
e.g., Anzer 1978; Mouschovias, & Poland 1978; Chen 1989; Vrsnak 1990;
Chen & Krall 2003). The fast progress of numerical techniques have recently enabled a very advanced
modeling of such a system, also providing the inclusion of magnetic field reconnection (e.g., Amari et al. 2000; Amari et al. 2003; Roussev et al. 2003; Kliem et al. 2004; Török & Kliem 2005; Birn et al. 2006; Gibson & Fan 2006;
for a review see Gibson et al. 2006). From the point of view of projection effects, it is important
to note that this class of models, based on the magnetic field configuration proposed by Titov &
Demoulin (1999), is not axi-symmetric, so the approximation in terms of the cone geometry is not
appropriate. Consequently, the projected width of the CME depends not only on the location of the source
region, but also on the orientation of the plane containing the flux-rope axis (see, e.g., Fig. 15 of
Cremades & Bothmer 2004). Similarly, the relationship between the plane-of-sky velocity and the
source-region position depends on the flux-rope orientation. Thus, again we find a much more complex
situation than in the cone geometry, certainly leading to the degradation of the W-bin based correlations
and, in particular, the
dependence. Finally, it should be noted that these
numerical simulations reveal significant morphological changes caused by kinking of the flux rope axis and by
reconnection, additionally degrading the
correlation.
As a conclusion, it is not surprising that the correlation of the plane-of-sky velocity and the source-region position is much weaker than expected from the simple cone model, since real CMEs appear in a broad variety of types and shapes and are generally much more complex than represented by any of actual models.
Acknowledgements
This work was sponsored by the Air Force Office of Scientific Research, USAF, under grant number FA8655-06-1-3036. We are thankful to the LASCO-SOHO and GOES teams for operating the instruments and performing the basic data reduction. We are especially grateful to Nat Gopalswamy, Seiji Yashiro, Grzegorz Michaek, and their colleagues for compiling the online LASCO CME Catalog.
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Figure 6: The ratio of the plane-of-sky velocity v and the true velocity v*, presented as a function of the source-region position, derived from a) model A, b) model B, c) model C. |
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The relationship between the plane-of-sky velocity v and the true velocity v* depends on the CME
geometry. In this paper we consider three different CME cone models frequently used in CME studies. At the
top of the cone model A has a spherical surface concentric with the solar surface, model B has a half-sphere,
whereas in model C a spherical surface is matched tangentially to the cone surface (see, e.g., Fig. 9 of
Schwenn et al. 2005). Models A, B, and C relate the plane-of-sky velocity v and the true
velocity v* as:
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(2) |
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(3) |
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(4) |
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(5) |
Figure 6 shows that the projection effect should be larger for narrower CMEs; i.e., the slopes of v/v* are steeper. The ratio of the true velocity v* and the observed velocity v is highest in model C and lowest in model A.