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Table 1

Parameters for the example objects.

Constant Earth-Moon Jupiter-Io V636 Cen.

Rc(m) 6.37 × 106a 6.99 × 107a 7.08 × 108b
Rco(m) 3.47 × 106c 5.71 × 107c ...
mc(kg) 5.97 × 1024c 1.90 × 1027c 2.09 × 1030b
acp(m) 3.84 × 108c 4.22 × 108c 9.57 × 109d
mp(kg) 7.35 × 1022c 8.91 × 1022c 1.70 × 1030b
L(W) ... 3.34 × 1017e 4.31 × 1026b
νm(m2s-1) 1.4 × 10-6f 3 × 10-7e 10-4g
Ωspin(day-1) 2π 2π/0.41h 2π/3.96 i
ΩP(day-1) 2π/27.32 2π/1.77h 2π/4.28b
Ω 0.0380 0.305 12.40
ϵ 2.8 × 10-8 1.1 × 10-7 1.6 × 10-4
E m 1.6 × 10-15 5.2 × 10-19 1.1 × 10-17
β ... 1.5 18
s e ... 2 1
E turb ... 1.6 × 10-13 6.3 × 10-5
σ ud 1.6 × 10-8 5.1 × 10-8 4.4 × 10-5
Dm n.s. 4.2 × 10-8 9.4 × 10-10 4.4 × 10-8
Dm f.s. ... 2.6 × 10-13 4.1 × 10-14
Dturb n.s. ... 5.3 × 10-7 0.11
Dturb f.s. ... 8.3 × 10-8 0.24

Notes. νm is the molecular viscosity, Em the Ekman number based only on the molecular viscosity, and Eturb the Ekman number based on the turbulent viscosity (the molecular viscosity is negligible in comparison to the turbulent one in these examples). Dm and Dturb are damping constants based on the molecular viscosity and the turbulent viscosity; n.s. and f.s. stand for no slip and free slip boundary conditions.

Reference.

(d)

calculated according to Kepler’s third law, with values given in Clausen et al. (2009);

(i)

calculated according to v = Ωspin·Rc with v the equatorial velocity given in Clausen et al. (2009).

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