Abstract. Oxidative processing of aircraft turbine-engine exhausts was studied using a
potential aerosol mass (PAM) chamber at different engine loads corresponding
to typical flight operations. Measurements were conducted at an engine test
cell. Organic gases (OGs) and particle emissions pre- and post-PAM
were measured. A suite of
instruments, including a proton-transfer-reaction mass spectrometer (PTR-MS)
for OGs, a multigas analyzer for
CO, CO2, NOx, and an aerosol mass spectrometer (AMS) for
nonrefractory particulate matter (NR-PM1) were used. Total aerosol mass
was dominated by secondary aerosol formation, which was approximately
2 orders of magnitude higher than the primary aerosol. The chemical
composition of both gaseous and particle emissions were also monitored at
different engine loads and were thrust-dependent. At idling load (thrust
2.5–7 %), more than 90 % of the secondary particle mass was organic
and could mostly be explained by the
oxidation of gaseous aromatic species, e.g., benzene; toluene; xylenes; tri-, tetra-, and
pentamethyl-benzene; and naphthalene. The oxygenated-aromatics, e.g., phenol,
furans, were also included in this aromatic fraction and their oxidation
could alone explain up to 25 % of the secondary organic particle mass at
idling loads. The organic fraction decreased with thrust level, while the
inorganic fraction increased. At an approximated cruise load sulfates
comprised 85 % of the total secondary particle mass.