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Two-sided ignition of a thin PMMA sheet in microgravity

机译:单面点火在微匍匐中的薄PMMA表

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Numerical computations and a series of experiments were conducted in microgravity to study the ignition characteristics of a thin polymethylmethacrylate (PMMA) sheet (thicknesses of 0.2 and 0.4 mm) using a CO_2 laser as an external radiant source. Two separate ignition events were observed, including ignition over the irradiated surface (frontside ignition), and ignition, after some delay, over the backside surface (backside ignition). The backside ignition was achieved in two different modes. In the first mode, after the laser was turned off, the flame shrank and stabilized closer to the fuel surface. This allowed the flame to travel from the frontside to the backside through the small, open hole generated by the laser's vaporization of PMMA. In the second mode, backside ignition was achieved during the laser irradiation. The numerical calculation simulating this second process predicts fresh oxygen supply flows from the backside gas phase to the frontside gas phase through the open hole, which mixes with accumulated hot MMA fuel vapor which is ignited as a second flame in the frontside gas phase above the hole. Then, the flame initiated from the second ignition travels through the hole to ignite the accumulated flammable mixture in the backside gas phase near the hole, attaining backside ignition. The first backside ignition mode was observed in 21% oxygen and the second backside ignition mode in 35%. The duration of the laser irradiation appears to have important effects on the onset of backside ignition. For example, in 21% oxygen, the backside ignition was attained after a 3 s laser duration but was not observed after a 6 s laser duration (within the available test time of 10 s). Longer laser duration might prevent two-sided ignition in low oxygen concentrations.
机译:使用CO_2激光作为外辐射源,在微匍匐基质中进行数值计算和一系列实验,以研究使用CO_2激光作为外辐射源的薄聚甲基丙烯酸甲酯(PMMA)片(PMMA)片(厚度为0.2和0.4mm的厚度。观察到两个单独的点火事件,包括在照射表面(前侧点火)上点火,并在后侧表面(背面点火)上的某些延迟之后点火。背面点火以两种不同的模式实现。在第一模式中,在截止激光之后,火焰缩短并稳定更靠近燃料表面。这允许火焰从前面行驶到通过激光器的PMMA蒸发产生的小型开孔,从前侧移动到后侧。在第二模式中,在激光照射期间实现了背面点火。模拟该第二过程的数值计算预测通过开孔从背面气相到前侧气相流动的新鲜氧气供应,其与累积的热MMA燃料蒸汽混合,在孔上方的前侧气相中被点燃为第二火焰。然后,从第二点火开始发起的火焰穿过孔,以在孔附近的背面气相中点燃累积的易燃混合物,达到背面点火。在35%的35%中以21%的氧气和第二个背面点火模式观察到第一后侧点火模式。激光照射的持续时间似乎对背面点火的开始具有重要影响。例如,在21%的氧气中,在3秒的激光持续时间后,在6秒的激光持续时间(在10秒的可用测试时间内之后未观察到后侧点火。更长的激光持续时间可能会在低氧浓度下防止双面点火。

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