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Table 1

Wave properties of studied CBFs.

Kinematics Dispersion Integrated intensity
Event Spacecraft v0 a d(Δr) / dr d(Δτ) / dt d(Itot) / dr
km s-1 m s-2 171 Å 195 Å

2007 May 19 Ahead 444 ± 75  −256 ± 134 0.3 ± 0.1 1.0 ± 0.2 1.08 ± 0.53 0.13 ± 1.07
Behind 447 ± 87  −260 ± 149 0.5 ± 0.1 1.1 ± 0.2 1.83 ± 0.41 0.24 ± 0.61
2007 Dec. 07 Ahead 270 ± 37  −152 ± 73 0.4 ± 0.1 1.0 ± 0.3 0.71 ± 0.37  −0.049 ± 0.002
Behind 247 ± 62  −117 ± 110 0.2 ± 0.2 0.8 ± 0.3 2.29 ± 0.41  −1.07 ± 0.12
2009 Feb. 12 Behind 405 ± 93  −291 ± 166 0.4 ± 0.2 2.0 ± 0.5  −3.27 ± 2.39  −0.59 ± 0.11
2009 Feb. 13 Behind 274 ± 53  −49 ± 34 0.4 ± 0.1 0.5 ± 0.1 4.33 ± 0.66  −0.74 ± 0.36

Notes. Kinematic values refer to the mean and standard deviation error of the bootstrapping parameter distributions. Dispersion and integrated intensity values refer to the rate of change of the relevant parameters, resulting from the linear fits shown in Figs. 12 and 16.

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