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Code Manual for CONTAIN 2.0 - Federation of American Scientists

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assumed to bum instantaneously if oxygen is available in the cell. This can only occur if oxygen is<br />

available during the same timestep when the hydrogen was produced. The rationale <strong>for</strong> this <<br />

approach is that the hydrogen is assumed to be near the surface <strong>of</strong> the drop during the same timestep<br />

during which it was produced. If oxygen is not available during this timestep, then it will only burn<br />

as governed by one <strong>of</strong> the other containment combustion models (deflagration, diffusion flame<br />

burning, or bulk spontaneous recombination). The hydrogen recombination reaction can also be<br />

disabled by the user in one or more cells by specifying RCOMH2 = OFF in the DHEAT or DCH-<br />

CELL input blocks.<br />

The hydrogen burning reaction is given by<br />

Hz+ 0.5 02+ HZO<br />

where 2.86 x 108Joules per kilogram-mole <strong>of</strong> hydrogen are released when hydrogen recombines<br />

with oxygen. This reaction is limited by the availability <strong>of</strong> oxygen in the cell and the amount <strong>of</strong><br />

hydrogen produced by DCH during the timestep. The energy released by the recombination process<br />

is added to the atmosphere, not the drop field, as shown in Equation (6-151).<br />

6.5 Heat Transfer<br />

Models are included <strong>for</strong> convective and radiative heat transfer between the debris and the<br />

atmosphere. The DCH radiation model also includes provisions <strong>for</strong> direct radiation from the debris<br />

to containment structures, including the pool and ice condenser. The first subsection below<br />

describes the convection model. The second subsection describes the DCH radiation model. The *<br />

models described below apply to debris in all fields, including the airborne fields and the nonairbome<br />

debris field.. The models do not apply to trapped debris that is transferred to the uppermost<br />

intermediate layer in the lower cell cavity. Heat transfer <strong>for</strong> debris in the lower cell is modeled as<br />

part <strong>of</strong> the lower cell heat transfer model as described in Chapter 5 and Section 10.6.<br />

6.5.1 Convective Heat Transfer<br />

Convection heat transfer from debris to gas is assumed to be by <strong>for</strong>ced convection. The heat transfer<br />

coei%cient is given by the Nusselt correlation <strong>of</strong> Ranz and Marshall [Ran52, Bir60] <strong>for</strong> <strong>for</strong>ced flow<br />

over a sphere<br />

‘Nu,, i. = <strong>2.0</strong> + 0.6 N#~ NPr,g 1’3<br />

(6-152)<br />

where N~ujJis the Nusselt number <strong>for</strong> debris field n in cell i. The convection heat transfer rate <strong>for</strong><br />

each debris field is individually calculated since each field has its own temperature, T~j$,and particle<br />

size, d..<br />

The N~,,~and NR,~parameters in this expression are calculated using gas properties at the boundary<br />

layer temperature, T~~,as recommended in Reference Bir60. The velocity, v,., is used as the <strong>for</strong>ced<br />

convection velocity in the Reynolds number. This velocity is calculated within the code from the ~<br />

Rev O 662 6/30/97

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