|Title||문석수, Essam Abo-Serie, 오희창, 배충식, "직접분사식가솔린 엔진용 고압스월분무의 액막두께 측정 및 해석", 한국액체미립화학회지, vol. 12, No. 4, pp211-219, 2007.12|
문석수, Essam Abo-Serie, 오희창, 배충식, “직접분사식가솔린 엔진용 고압스월분무의 액막두께 측정 및 해석”, 한국액체미립화학회지, vol. 12, No. 4, pp211-219, 2007.12
The liquid film thickness inside a pressure-swirl nozzle was measured, and then the measured liquid film thickness was compared with the results from previous empirical equations. The liquid film inside the nozzle was visualized using extended transparent nozzles and a microscopic imaging system, and then the measurement error was evaluated using optical geometry analysis. The high injection pressures up to 7MPa were adopted to simulate the injection conditions of the direct-injection spark-ignition engines. The totally different tow injectors with different fuels, nozzle lengths, nozzle diameters and swirlers were utilized to obtain the comprehensive equations. The results showed that the liquid film thickness very slightly decreased at high injection pressures and the empirical equations overestimated the effect of injection pressure. Most of empirical equations did not include the effect of nozzle length and swirler angle, although it caused significant change in liquid film thickness. A new empirical equation was suggested based on the experimental results with the effects of fuel properties, injection pressure, nozzle diameter, nozzle length and swirler angle.