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Table 5 Alternative Rm numbers

From: Magnetic field stretching at the top of the shell of numerical dynamos

Model

\(\cos \gamma \)

\(Rm_{\text {a}}\)

\(Rm_{\text {s}}\)

\(\xi _{Rm}\)

\(Rm_{\text {e}}\)

Rm

1

0.65

88.37

49.22

0.65

89.98

137

2

0.65

166.77

80.55

0.68

167.44

255

3

0.66

146.20

89.88

0.66

155.15

219

4

0.59

48.71

45.10

0.59

55.44

82

5

0.64

79.88

60.78

0.61

86.51

125

6

0.66

155.15

104.72

0.65

169.17

234

7

0.64

80.01

75.93

0.60

93.72

126

8

0.65

140.70

100.18

0.63

151.66

218

9

0.66

294.81

192.80

0.66

321.33

446

  1. \(\cos \gamma \) is the field–flow alignment factor. \(Rm_{\text {a}}\) and \(Rm_{\text {s}}\) are the advective and stretching effective magnetic Reynolds numbers, respectively. The effective magnetic Reynolds number \(Rm_{\text {e}}\) was calculated using the advection/stretching interference factor \(\xi _{Rm}\). For comparison the conventional Rm number is reproduced from Table 1