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

6.3 Fuel tank temperatures and ambient pressure for a flight profile test up to
30,000’ altitude 51
6.4 Calculated temporal mass transport occurring within the fuel tank for a
flight profile test up to 30,000’ altitude 51
6.5 Temporal change in FAR for a heated fuel tank at sea level with constant
ambient temperature and lower flammability range [26] 55
6.6 Temporal change in calculated Le Chatelier’s ratio calculated for two fuels
with flashpoints of 115°F and 120°F for a heated fuel tank at sea level and
Le Chatelier’s flammability limit [27] 55
6.7 Liquid temperature effects on mixture flammability using the FAR rule [26];
heated tank at sea level with constant ambient temperature and pressure 56
6.8 Liquid temperature effects on mixture flammability using Le Chatelier’s
flammability rule [27]; heated tank at sea level with constant ambient
temperature and pressure 56
6.9 Mass loading effects on mixture flammability using the FAR rule [26];
heated tank at sea level with constant ambient temperature and pressure 57
6.10 Mass loading effects on mixture flammability using Le Chatelier’s
flammability rule [27]; heated tank at sea level with constant ambient
temperature and pressure 57
6.11 Temporal change in FAR for a flight profile test up to 30,000’ altitude and
range of the lower flammability limit [26] 60
6.12 Calculated Le Chatelier’s ratio for a flight profile test up to 30,000’ altitude
and Le Chatelier’s flammability limit [27] 60
6.13 Liquid fuel temperature effects on flammability using the FAR rule [26];
flight profile test up to 30,000’ altitude 61
6.14 Liquid fuel temperature effects on flammability using Le Chatelier’s
flammability rule [27]; flight profile test up to 30,000’ altitude 61
6.15 Mass loading effects on flammability using the FAR rule [26]; flight profile
test up to 30,000’ altitude 62
6.16 Mass loading effects on flammability using Le Chatelier’s flammability
rule [27]; flight profile test up to 30,000’ altitude 62
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