Current research by the US Air Force and Navy is concentrating on
obtaining detonations in a pulse detonation engine (PDE) with low
vapor pressure, kerosene based jet fuels. These fuels have a low
vapor pressure and the performance of a liquid hydrocarbon fueled
PDE is significantly hindered by the presence of fuel droplets. A
high pressure, fuel flash vaporization system (FVS) has been
designed and built to reduce and eliminate the time required to
evaporate the fuel droplets. Four fuels are tested: n-heptane,
isooctane, aviation gasoline, and JP-8. The fuels vary in
volatility and octane number and present a clear picture on the
benefits of flash vaporization. Results show the FVS quickly
provided a detonable mixture for all of the fuels tested without
coking or clogging the fuel lines. Combustion results validated the
model used to predict the fuel and air temperatures required to
achieve gaseous mixtures with each fuel. The most significant
achievement of the research was the detonation of flash vaporized
JP-8 and air. The results show that the flash vaporized JP-8 used
20 percent less fuel to ignite the fuel air mixture twice as fast
(8 ms from 16 ms) when compared to the unheated JP-8 combustion
data.
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