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

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30,000’, respectively. The same two fuel compositions with flashpo<strong>in</strong>ts <strong>of</strong> 115°F and<br />

120°F were used for the calculations. As with the previously presented constant pressure<br />

data, the results show that the calculated vapor concentration pr<strong>of</strong>iles bracketed the<br />

measured vapor concentration pr<strong>of</strong>ile, <strong>in</strong>dicat<strong>in</strong>g that the model provided a reasonably<br />

accurate prediction <strong>of</strong> fuel vaporization under vary<strong>in</strong>g ambient conditions.<br />

Temperature, Deg. F.<br />

120<br />

100<br />

80<br />

60<br />

40<br />

20<br />

0<br />

Thermocouple<br />

Error<br />

Liquid <strong>Fuel</strong> Temp<br />

Average Ullage Temp<br />

Average Surface Temp<br />

Ambient Pressure<br />

0 2000 4000 6000 8000<br />

Time, seconds<br />

Figure 5.13. Test FLT-10: simulated flight with cruise at 10,000’ altitude; fuel tank temperatures<br />

and ambient pressure.<br />

20<br />

15<br />

10<br />

5<br />

0<br />

Pressure, psia<br />

43

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