Vaporization of JP-8 Jet Fuel in a Simulated Aircraft Fuel Tank ...
Vaporization of JP-8 Jet Fuel in a Simulated Aircraft Fuel Tank ...
Vaporization of JP-8 Jet Fuel in a Simulated Aircraft Fuel Tank ...
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1.3 Objectives <strong>of</strong> the Thesis<br />
The ultimate goal for fuel tank protection research is to determ<strong>in</strong>e methods, or<br />
procedures, that can elim<strong>in</strong>ate the possibility <strong>of</strong> fuel tank fires and explosions. <strong>Fuel</strong><br />
vaporization model<strong>in</strong>g can be used to estimate the fuel vapor concentration <strong>in</strong> the ullage<br />
<strong>of</strong> a fuel tank as a function <strong>of</strong> the tank pressure and temperature. Such a model can be<br />
valuable to the fuel tank protection cause, as computer model<strong>in</strong>g reduces the cost and<br />
time <strong>of</strong> full-scale experimentation. The model calculations can also be used for fuel tank<br />
<strong>in</strong>ert<strong>in</strong>g requirements or to verify the <strong>in</strong>tr<strong>in</strong>sic safety <strong>of</strong> an <strong>in</strong>ert fuel tank. The objective<br />
<strong>of</strong> this study is to generate experimental data on fuel vaporization for tank conditions<br />
appropriate to those encountered <strong>in</strong> an aircraft fuel tank. The data obta<strong>in</strong>ed can then be<br />
available for validat<strong>in</strong>g the estimations from vaporization models.<br />
To that effect, an experiment was designed to simulate an <strong>in</strong>-flight environment<br />
around a fuel tank and measure tank conditions. The experimental setup consisted <strong>of</strong> a<br />
simulated fuel tank with a uniformly heated floor surface and unheated sidewalls and top<br />
surface. The tank was <strong>in</strong>strumented with thermocouples and a total hydrocarbon detector<br />
for measur<strong>in</strong>g the vapor concentration <strong>in</strong> the ullage gas. The fuel tank was situated <strong>in</strong> an<br />
environmental chamber that could vary the ambient pressure and temperature to simulate<br />
flight conditions. Data was collected for different pressure and temperature conditions<br />
us<strong>in</strong>g <strong>JP</strong>-8 as the evaporat<strong>in</strong>g liquid. A limited number <strong>of</strong> tests were also performed<br />
us<strong>in</strong>g isooctane (2-2-4 trimethylpentane) as the test liquid. The data was compared with<br />
predictions from an available fuel vaporization model [11] that was also used to assess<br />
the flammability <strong>of</strong> the vapor generated and for discussion <strong>of</strong> the overall transport<br />
processes occurr<strong>in</strong>g with<strong>in</strong> the fuel tank.<br />
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