采用微细热电偶、红外热像仪、CCD摄像及纹影技术对不同初始温度航空煤油表面火蔓现象及机理进行实验研究.结果表明:当航空煤油(开杯闪点为66,℃)的初始温度T0≤82.5,℃时,其火焰蔓延主要受液相控制,在此阶段表面流预热作用是火焰脉动蔓延的主要控制机制,火焰蔓延平均速度随初始温度升高呈指数增长关系;当航空煤油初始温度T0〉82.5,℃时,其火焰蔓延主要受气相控制,火焰蔓延速度依赖于油面上方蒸气浓度.
Fine thermocouples,infrared thermograph,CCD cameras and schlieren system were applied to study the characteristics and mechanisms of flame spread over aviation kerosene(open cup flash point is 66,℃).Two control-ling mechanisms were found.For initial temperature T0≤82.5,℃,flame spread was mainly controlled by liquid phase.During the period,surface flow is the main cause for oscillatory regime,and the average flame spread rate increases exponentially with the increase of initial temperature.For initial temperature T0〉82.5,℃,flame spread was mainly controlled by gas phase,and flame spread rate was dependent on the concentration of fuel vapor above liquid surface.