The
fine particulate matter (PM) emissions from the use of two
types of Fischer–Tropsch aviation fuels and their 50:50 blends
with military JP-8 were quantified as part of the first Alternative
Aviation Fuel Experiment (AAFEX). Measurements were made 30-m downstream
of a CFM56-2C1 engine for PM mass and number, particle size distribution,
black carbon (BC), and volatile PM (sulfate + organics) using selected
online instrumentation. The PM number emission index (EIN) ranged from ∼2 × 1015 to 7 × 1016 particles/kg fuel burned depending on fuel flow, fuel composition,
and sampling temperature with the magnitude of the emissions inversely
correlated to fuel flow. The PM mass emissions (EIM) measured
in the study varied from ∼5 to 680 mg/kg fuel, again depending
on fuel flow, fuel type, and sampling temperature with a characteristic
U-shaped curve of EIM with respect to fuel flow observed
from the data. At low fuel flow (corresponding to low engine power),
particle number and volume size distributions contained a single mode,
whereas at higher engine power, a bimodal distribution was observed.
The BC emissions varied from ∼3 to 415 mg/kg fuel depending
on fuel type and were found to exponentially increase with engine
power (fuel flow). The volatile PM varied with sample temperature,
fuel type, and increasing fuel flow within the range of EIs from ∼0.4
to 11 mg/kg fuel with the highest values being at low fuel flow. Finally,
the use of the two neat alternative fuels reduced the EIN by a median value of 70–73% and the EIM by ∼94%
as compared to JP-8 across all power conditions tested.