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

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For the 30,000’ altitude data, the chamber was therefore <strong>in</strong>itially cooled so that the <strong>in</strong>itial<br />

fuel temperature was about 40°F while the maximum liquid temperature was kept below<br />

approximately 60°F to reduce the fuel vapor pressure so that the ullage vapor<br />

concentrations rema<strong>in</strong>ed with<strong>in</strong> the calibration range.<br />

Temperature, Deg. F.<br />

140<br />

120<br />

100<br />

80<br />

60<br />

40<br />

20<br />

0<br />

Thermocouple<br />

Error<br />

0 1000 2000 3000 4000<br />

Time, seconds<br />

FID Error<br />

Liquid Temp<br />

Measured THC<br />

Calculated THC, 115 FP<br />

Calculated THC, 120 FP<br />

Figure 5.10. <strong>Fuel</strong> heat<strong>in</strong>g at 10,000’ altitude, 10.2 psia; <strong>in</strong>put fuel temperature and comparison <strong>of</strong><br />

calculated and measured ullage vapor concentrations, M.L.=31.5kg/m 3 .<br />

Temperature, Deg. F.<br />

120<br />

100<br />

80<br />

60<br />

40<br />

20<br />

0<br />

Thermocouple<br />

Error<br />

FID Error<br />

Liquid Temp<br />

Measured THC<br />

Calculated THC, 115 FP<br />

Calculated THC, 120 FP<br />

0 1000 2000 3000 4000<br />

Time, seconds<br />

Figure 5.11. <strong>Fuel</strong> heat<strong>in</strong>g at 20,000’ altitude, 6.9 psia; <strong>in</strong>put fuel temperature and comparison <strong>of</strong><br />

calculated and measured ullage vapor concentrations, M.L.=31.5kg/m 3 .<br />

4<br />

3.5<br />

3<br />

2.5<br />

2<br />

1.5<br />

1<br />

0.5<br />

0<br />

5<br />

4<br />

3<br />

2<br />

1<br />

0<br />

% Propane Equivalent<br />

% Propane Equivalent<br />

41

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