[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 | ||||||
---|---|---|---|---|---|---|---|
5-methyl-2-hexanol | A | ||||||
5-methyl-2-hexanol | B | ||||||
methyl-m-toluate | A | ||||||
methyl-m-toluate | B | ||||||
glycerol | A | ||||||
glycerol | B |
[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 .