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Heat and Gas Diffusion in Comet Nuclei (pdf file 5.5 MB) - ISSI

Heat and Gas Diffusion in Comet Nuclei (pdf file 5.5 MB) - ISSI

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6.4. Simultaneous Solution for Transfer of <strong>Heat</strong> <strong>and</strong> Mass 109<br />

<strong>and</strong> the total production rate is obta<strong>in</strong>ed by summ<strong>in</strong>g the contributions of<br />

such wedges over one sp<strong>in</strong> period. This is, essentially, a 2.5-dimensional<br />

calculation. The next step is to take <strong>in</strong>to account both diurnal <strong>and</strong> latitud<strong>in</strong>al<br />

solar flux variations (Huebner <strong>and</strong> Boice, 1992; Gutiérrez et al.,<br />

2000; Julian et al., 2000; Cohen et al., 2003, De Sanctis et al., 2005), consider<strong>in</strong>g,<br />

however, only radial heat conduction, that is, neglect<strong>in</strong>g lateral<br />

conduction. This quasi 3-D approach is amply justified by the extremely<br />

low heat conductivity of cometary material; the characteristic heat diffusion<br />

time between equator <strong>and</strong> pole (as between surface <strong>and</strong> centre) is of<br />

the order of the life-time of a comet (see Table 5.1 above). The different<br />

models are shown schematically <strong>in</strong> Fig. 6.4; however, calculations use much<br />

f<strong>in</strong>er meshes than the ones shown.<br />

6.4 Simultaneous Solution for Transfer of <strong>Heat</strong><br />

<strong>and</strong> Mass<br />

We note that the evolution equations are coupled through the source terms<br />

<strong>and</strong> the gas fluxes, which are functions of both temperature <strong>and</strong> pressure,<br />

<strong>and</strong> hence must be solved simultaneously. A flowchart of an evolution code<br />

that uses an implicit numerical scheme is shown <strong>in</strong> Fig. 6.5; the energy <strong>and</strong><br />

mass balance equations are solved <strong>in</strong> an alternat<strong>in</strong>g sequence, until they<br />

converge. The question marks represent the question whether convergence<br />

has been achieved <strong>in</strong> the correspond<strong>in</strong>g process. The question mark follow<strong>in</strong>g<br />

n or m represents the question whether the number of iterations has<br />

exceeded the allowed limit (s<strong>in</strong>ce there is no po<strong>in</strong>t <strong>in</strong> cont<strong>in</strong>u<strong>in</strong>g an iterative<br />

process that does not converge).<br />

The simultaneous solution of the heat <strong>and</strong> mass conservation equations is<br />

extremely time consum<strong>in</strong>g, keep<strong>in</strong>g <strong>in</strong> m<strong>in</strong>d that the equations are strongly<br />

nonl<strong>in</strong>ear. Simplify<strong>in</strong>g approximations may be used under special conditions.<br />

If the effective permeability of the medium is sufficiently high, the left<br />

side of the mass conservation equation for the gas phases (Eq. 4.9) becomes<br />

negligible. Neglect<strong>in</strong>g it is tantamount to a quasi-steady state approximation,<br />

where gas densities <strong>and</strong> production rates change only as far as the<br />

temperature distribution changes. Thus Eqs. (4.9 – 4.11) are replaced by<br />

∇ · J n = q n<br />

∂ρ s,n<br />

∂t<br />

= −q n (6.23)<br />

In this way we have to solve only one time-dependent equation, supplemented<br />

by structure (space-dependent) equations. This constitutes a large<br />

computational advantage, particularly <strong>in</strong> a long-term evolution calculation,

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