In
this work, military jet fuel JP-5 surrogates were formulated
and tested in comparison to a nominal JP-5 fuel. Combustion experiments
were conducted in an advanced engine technology (AET) ignition quality
tester (IQT) and a Yanmar L100W Tier 4 diesel engine due to the potential
use of jet fuel in diesel engines in military situations. The surrogate
development process began with determining the fuel chemical composition
based on analyses of 256 JP-5 fuel samples. The physical and chemical
properties of density, viscosity, flash point, surface tension, speed
of sound, and distillation behavior guided the selection of the surrogate
components and their composition. JP-5 differs from other aviation
fuels in its properties, but most importantly in flash point, which
is higher for safety purposes. Surrogates were prepared from n-dodecane, n-butylbenzene, 1-methylnaphthalene,
tetralin, trans-decalin, iso-cetane,
and n-butylcyclohexane as representatives of seven
of the nine major chemical categories found in jet fuel. The mass
fraction of each compound in the surrogates that fell within the range
for that chemical class was found in real JP-5 fuels. After optimizing
the surrogates for physical and chemical properties, six surrogates
were selected for combustion testing in the Yanmar diesel engine,
one of which was specifically selected for a low-derived cetane number
(DCN). This surrogate performed poorly in the Yanmar engine. Four
of the remaining five surrogates performed similarly to the baseline
JP-5 in the diesel engine in terms of values and variability of ignition
delay, rate of heat release, peak pressure, and the crank angle at
which 50% of the fuel is burned. Of the six surrogates tested, the
best one in terms of physical properties, chemical properties, and
combustion behavior was the one that contained 0.2421, 0.1503, 0.0500,
0.0141, 0.0121, 0.2532, and 0.2782 mass percentages of n-dodecane, n-butylbenzene, 1-methylnaphthalene,
tetralin, trans-decalin, iso-cetane,
and n-butylcyclohexane, respectively.