[page 1287, §1]
[1287.1.1] Because the data have been fitted at different temperatures we are able
to observe the temperature dependence of the fitting parameters.
[1287.1.2] For and
we perform Vogel-Tammann-Fulcher fits
provided by equation (13).
[1287.1.3] From the fits we obtain the Vogel-Fulcher temperatures
and
as well as the fragility parameters
and
for the relaxation times
and
for model A and model B (see Table 2).
material | model | ![]() |
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5-methyl-2-hexanol | A | ![]() |
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5-methyl-2-hexanol | B | ![]() |
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methyl-m-toluate | A | ![]() |
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methyl-m-toluate | B | ![]() |
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glycerol | A | ![]() |
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glycerol | B | ![]() |
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[1287.2.1] For all fits we see a temperature dependence of the
relaxation times and
(Fig. 4 - Fig. 6)
that follows the Vogel-Tammann-Fulcher fitting function remarkably well.
[1287.2.2] The relaxation times also show a clear downward trend as the
temperature increases, which confirms that
,
and
are physically
meaningful and can be interpreted as relaxation times
even tough they appear with a non-integer power in equations
(11) and (12).
[1287.3.1] The parameters ,
and
also
show a temperature dependence.
[1287.3.2] In the case of 5-methyl-2-hexanol (Fig. 4)
there is an increase of
with temperature until a plateau
near
is reached.
[1287.3.3] This effect comes from the decreasing slope of the excess wing with
increasing temperature.
[1287.3.4] In the fitting function of model A this behavior can be achieved by
increasing
.
[1287.3.5] For the same material there is an apparent increase of
between
(
) and
(
)
which has the same origin as the increase in
in model A.
[1287.3.6] By increasing
the excess wing becomes less steep.
[1287.3.7] The plateau at
(
) and above comes
from the fact that the fits at those
temperatures are done mainly for the
-peak,
because the excess wing is not visible.
[1287.4.1] For methyl-m-toluate and glycerol there is also a clear temperature dependence
of ,
and
(Fig. 5 and Fig. 6).
[1287.4.2] The trend is however reversed in comparison to 5-methyl-2-hexanol.
[1287.4.3] This comes from the increasing slope of the excess wing with
increasing temperature.
[1287.4.4] This behavior can be achieved in the fit functions by decreasing
,
respectively
.
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