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Vaporization of JP-8 Jet Fuel in a Simulated Aircraft Fuel Tank ...

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APPENDIX A: REVIEW OF FUEL VAPORIZATION MODEL<br />

The model used <strong>in</strong> this thesis is presented <strong>in</strong> reference [11] and will be summarized here<br />

<strong>in</strong> the appendix.<br />

Several pr<strong>in</strong>cipal assumptions were made <strong>in</strong> the model to simplify the<br />

calculations. The flow field <strong>in</strong> the tank was assumed driven entirely by natural<br />

convection between the heated liquid fuel on the tank floor and the unheated tank ceil<strong>in</strong>g<br />

and sidewalls. The ullage gas was considered well mixed with no thermal or<br />

concentration gradients exist<strong>in</strong>g with<strong>in</strong> the ullage, which was justified by the fact that the<br />

natural convection flow <strong>in</strong> the tank was <strong>in</strong> the turbulent region, s<strong>in</strong>ce the magnitude <strong>of</strong> the<br />

Raleigh number, based on the floor to ceil<strong>in</strong>g temperature difference and the distance<br />

between them, was typically <strong>of</strong> order (10 9 ).<br />

Initially it was assumed that the ullage gas mixture would be composed <strong>of</strong> N<br />

species, consist<strong>in</strong>g <strong>of</strong> N-1 fuel vapor components and atmospheric air. As the species<br />

concentrations were low for the purposes <strong>of</strong> these experiments, the vaporization rate <strong>of</strong><br />

the fuel species considered was expressed by the relationship:<br />

( y − y ) , i = → N<br />

65<br />

m ei = A1hi<br />

ρ fi gi 1<br />

( 1 )<br />

The analogy between heat and mass transfer allowed for the species Sherwood number to<br />

be expressed <strong>in</strong> terms <strong>of</strong> the Nusselt number:<br />

1/<br />

3<br />

Pr ⎟ hi<br />

L ⎛ Sci<br />

⎞<br />

Sh i = = Nu⎜<br />

( 2 )<br />

D ⎝ ⎠<br />

On the horizontal surfaces the Nusselt number was found by [38]:<br />

i<br />

( ) 3 / 1<br />

Nu = 0. 14 Ra<br />

( 3 )

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