|Title||문석수, Essam Abo-Serie, 최재준, 배충식, "고압스월분무 액막유동의 초기 발달과정에 대한 연구," 한국액체미립화학회지, vol. 11, No. 4, pp212-219, 2006. 12.|
문석수, Essam Abo-Serie, 최재준, 배충식, “고압스월분무 액막유동의 초기 발달과정에 대한 연구,” 한국액체미립화학회지, vol. 11, No. 4, pp212-219, 2006. 12.
The initial film flow development of the high-pressure swirl spray was investigated at different injector operating conditions to analyze film flow development and to provide the input data for the modeling works. This result can be also useful to verify the previously simulated results. The initial flow conditions such as liquid film thickness, flow angle and flow divergence are obtained by visualizing the inside and near the nozzle flow with a microscopic imaging system. The visualized images are quantified using an image processing tool. From the information of liquid film thickness and flow angle, the initial axial and tangential velocity and the swirl number of the swirl spray are successfully determined at various operating conditions. The experimental results showed that the initial liquid film thickness, flow angle and flow divergence are remained constant when the injection pressure is increased. However, initial film conditions are severely changed when the fuel temperature is increased. The swirl number remained constant when the injection pressure is increased while it showed increased value at high fuel temperature condition.
|Previous||염기태, 장진영, 배충식. “가솔린 예혼합 압축 착화 엔진의 농후 한계에서 연소와 노킹 특성”, 한국자동차공학회 논문집, vol. 14, No. 6, pp9-16, 2006. 11.|
|Next||국상훈, 공장식, 박세익, 배충식, 김장헌, “분사각 및 분공 직경이 예혼합 압축착화 엔진 연소에 미치는 영향”, 한국자동차공학회 논문집, vol. 15, No. 2, pp1-7, 2007. 3.|