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AUTOIGNITION AND COMBUSTION OF A FUEL DROPLET ARRAY AT HIGH PRESSURES UNDER MICROGRAVITY

机译:小压力下燃料液滴阵列的自燃和燃烧

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An experimental study has been performed under microgravity condition to obtain the detailed information needed for the deep understanding of the combustion phenomena of fuel droplet arrays, which autoignite in supercritical gaseous environment. The microgravity environment aboard the capsule of the drop shaft at MGLAB was utilized for the experiments. The droplet array suspended at the tip of fine quartz fibers in the cold section of the high-pressure combustion chamber was transferred quickly to be subjected to a hot gaseous medium in an electric furnace. This resulted in evaporation, autoignition and combustion of the droplet array in high-pressure and high-temperature gaseous environment. The ignition delay increased a little and the pressure effect on the ignition delay decreased with a decrease of the droplet spacing. The burning time increased monotonically with a decrease of the droplet spacing. The time period of the early stage of droplet heating was longer and the evaporation rate was lower with smaller droplet spacing. A distance between the droplet array and the outer edge of the flame formed around the droplet array was larger with smaller droplet spacing.
机译:在微匍匐条件下进行了实验研究,以获得深度理解燃料液滴阵列的燃烧现象所需的详细信息,该燃料液滴阵列中的超临界气态环境中的自燃。在MGlAb上的掉落轴的胶囊上的微匍匐环境用于实验。液滴阵列在高压燃烧室的冷截面中悬浮在高压燃烧室的冷截面中的尖端被快速转移到电炉中进行热气态介质。这导致高压和高温气体环境中液滴阵列的蒸发,自燃和燃烧。点火延迟增加一点,随着液滴间隔的减小,点火延迟的压力效应降低。燃烧时间随着液滴间隔的减小而单调地增加。液滴加热早期阶段的时间段更长,蒸发速率较小,液滴间距较低。液滴阵列与围绕液滴阵列形成的火焰的外边缘之间的距离较大,具有较小的液滴间距。

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