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In-cylinder temperature and velocity fields were quantified simultaneously in an optically accessible, small-bore diesel engine. A technique utilizing luminescence from Pr:YAG phosphor particles aerosolized into the intake air was used for temperature determination while particle image velocimetry (PIV) on the aforementioned phosphor particles was used to simultaneously measure the velocity field. The temperature and velocity fields were measured at different points throughout the compression stroke up to −30 CAD. Systematic interference due to emission from the piston window reduced the accuracy of the measurements at crank angles closer to TDC. Single-shot simultaneous measurements of the temperature and velocity fields were made using both unheated and heated intake temperatures. In both cases, cycle-to-cycle variations in the temperature and velocity fields were visible.

Planar laser-induced fluorescence of 3-pentanone doped into the fuel (iso-octane) and OH, which is present in the combustion products, was performed in an optically accessible direct-injection spark-ignition (DISI) engine under stratified and homogeneous operating conditions. A wall-guided, swirl-based combustion chamber was utilized, and experiments were performed for light load, where the fuel-air equivalence ratio was 0.3, and high load conditions, with an equivalence ratio of 0.7, at speeds of 600 and 1200 rpm. The 3-pentanone images were calibrated through the use of a premixed charge condition of known equivalence ratio, with corrections applied for number density changes due to combustion. At the light load condition combustion of the highly stratified fuel cloud was directly measured for the first time. The equivalence ratio of the mixture at the flame front was found to be in the range from 0.5 - 0.8 for optimized combustion conditions in this engine.

Optically-accessible engines are a key tool for the study of sprays, mixing, and ignition and combustion phenomena in internal combustion (IC) engines. Due to their construction, they are typically operated for limited durations, resulting in significant thermal transients in the in-cylinder surface temperatures and cycle-to-cycle in-cylinder gas temperature. This makes collection of highly repeatable data difficult and can introduce considerable uncertainty in the in-cylinder thermal conditions. In this paper, rigorous analyses of transient in-cylinder boundary conditions and in-cylinder gas temperature were performed in an optically-accessible compression-ignition engine. Piston surface thermometry, in-cylinder pressure measurements, and in-cylinder gas thermometry were employed to determine the engine warmup time required to reach a quasi-steady thermal state for motored operation over a range of intake air temperatures and pressures from 300-420 K and 100-300 kPa, respectively.