PLANAR LASER RAYLEIGH-SCATTERING FOR QUANTITATIVE VAPOR-FUEL IMAGING IN A DIESEL JET

Citation
C. Espey et al., PLANAR LASER RAYLEIGH-SCATTERING FOR QUANTITATIVE VAPOR-FUEL IMAGING IN A DIESEL JET, Combustion and flame, 109(1-2), 1997, pp. 65-86
Citations number
56
Categorie Soggetti
Engineering,"Energy & Fuels",Thermodynamics
Journal title
ISSN journal
00102180
Volume
109
Issue
1-2
Year of publication
1997
Pages
65 - 86
Database
ISI
SICI code
0010-2180(1997)109:1-2<65:PLRFQV>2.0.ZU;2-1
Abstract
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.