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

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7.0 CONCLUSIONS AND RECOMMENDATIONS<br />

The experimentation performed was successful <strong>in</strong> measur<strong>in</strong>g ullage vapor concentration<br />

<strong>in</strong> a simulated aircraft fuel tank exposed to vary<strong>in</strong>g ambient conditions. A large set <strong>of</strong><br />

data was collected that <strong>in</strong>cluded fuel vaporization test<strong>in</strong>g at constant ambient pressure<br />

and temperature, constant reduced ambient pressure, and flight pr<strong>of</strong>ile tests with vary<strong>in</strong>g<br />

ambient conditions appropriate to <strong>in</strong>-flight aircraft fuel tank conditions. The data was<br />

useful <strong>in</strong> validat<strong>in</strong>g fuel vaporization model calculations from a pre-exist<strong>in</strong>g model. The<br />

model calculations <strong>of</strong> ullage gas temperature and vapor concentration proved to be <strong>in</strong><br />

good agreement with experimentally measured data. The model was very useful <strong>in</strong><br />

describ<strong>in</strong>g the transport processes occurr<strong>in</strong>g with<strong>in</strong> the tank and evaluat<strong>in</strong>g the<br />

flammability <strong>in</strong> the experimental fuel tank. The flammability assessments <strong>in</strong>dicated that<br />

Le Chatelier’s rule was more conservative than the FAR rule, and that from a safety<br />

perspective the FAR rule should be used <strong>in</strong> differentiat<strong>in</strong>g between safe, non-flammable<br />

conditions and dangerously flammable conditions. The data generated has proven<br />

successful <strong>in</strong> validat<strong>in</strong>g a model and can be used for further validation work.<br />

Further detailed experimental data on <strong>JP</strong>-8 flammability limits is required for<br />

further model validation, as well as laboratory test<strong>in</strong>g <strong>in</strong> full sized aircraft fuel tanks and<br />

possibly test<strong>in</strong>g from a fully <strong>in</strong>strumented fuel tank <strong>in</strong> an <strong>in</strong>-flight aircraft. Actual fuel<br />

tank test<strong>in</strong>g would present several complications. <strong>Aircraft</strong> center w<strong>in</strong>g tanks are divided<br />

<strong>in</strong>to several different compartments that are connected via small open<strong>in</strong>gs <strong>in</strong> the<br />

partitions. This will complicate the <strong>in</strong>ternal flow field and possibly cause ullage gas<br />

stratification between the compartments. Also, it was seen <strong>in</strong> this work that the model<br />

calculations were heavily dependent upon the <strong>in</strong>put temperatures; therefore accurate<br />

63

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