Quantitative images of vapor-phase fuel concentrations were obtained i
n an evaporating and combusting diesel jet using planar laser Rayleigh
scattering. The diagnostic has been calibrated, evaluated, and succes
sfully applied to an optically accessible direct-injection diesel engi
ne for fired and nonfired operating conditions. The measurements were
obtained in the leading portion of the diesel jet (the zone beyond 27
mm from the injector nozzle), where the fuel is entirely evaporated, a
nd which corresponds to the main combustion zone in this engine. The t
echnique was shown to be effective for quantitative imaging of the fue
l-vapor concentration before ignition, with high spatial and temporal
resolution. Additionally, images of the fuel-vapor concentration were
further reduced to imagers of the equivalence ratio using an adiabatic
mixing assumption to model the local temperature of the evaporating d
iesel jet. This procedure also yielded temperature distribution images
. The results show that, at 4.5 degrees crank angle (0.63 ms) after th
e start of injection, which corresponds to the time just before the fi
rst indicated heat release, the fuel and air are relatively well mixed
in the leading portion of the diesel jet. At this crank angle, the eq
uivalence ratio in the majority of the jet ranges from 2 to 4. The edg
es of the jet are well defined, with the signal level rising sharply f
rom the background level up to levels corresponding to equivalence rat
ios in the jet. The temperature of the richest mixture regions in the
jet is as low as 700 K, with the ambient air temperature at 1000 K. Fi
nally, comparisons of Rayleigh images of the reacting and nonreacting
jet show that the initial breakdown of the fuel, indicated by a signif
icant decrease in the Rayleigh signal intensity, occurs throughout the
cross section of the leading portion of the diesel jet. (C) 1997 by T
he Combustion Institute.