Abstract High-energy density aviation fuels are tested to see feasibility as alternative fuels to conventional jet fuels. They are derivatives of the existing high-energy density hydrocarbon fuels, exo-tetrahydrodicyclopentadiene and exo-tetrahydrotricyclopentadiene.… Click to show full abstract
Abstract High-energy density aviation fuels are tested to see feasibility as alternative fuels to conventional jet fuels. They are derivatives of the existing high-energy density hydrocarbon fuels, exo-tetrahydrodicyclopentadiene and exo-tetrahydrotricyclopentadiene. Combustion properties and ignition delay times of these alternative fuels, called high performance fuels (HPF-1 and 2) are measured. Densities of HPF-1 and HPF-2 are similar to density of exo-tetrahydrodicyclopentadiene, but their H/C ratio, molecular weight, heat of combustion, derived cetane number, and threshold sooting index are quite higher than those of exo-tetrahydrodicyclopentadiene. It is found that HPF-1 and 2 have higher heat of combustion and lower sooting propensity than conventional jet aviation fuels when they are compared at the same fuel density. On the other hand, ignition delay time is measured in a temperature range from 950 K to 1,300 K at 12 atm by using a shock tube. Results show that ignition delay time of the two fuels is shorter than exo-tetrahydrodicyclopentadiene. HPF-2 containing methylcyclohexane has much shorter ignition delay time than exo-tetrahydrodicyclopentadiene at high temperature over 1,050 K.
               
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