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首页> 外文期刊>Microgravity science and technology >Effects of Spacing and Arrangement of Droplet on Combustion Characteristics of Monodispersed Suspended-Droplet Cluster Model under Microgravity
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Effects of Spacing and Arrangement of Droplet on Combustion Characteristics of Monodispersed Suspended-Droplet Cluster Model under Microgravity

机译:微重力下液滴的间距和排列对单分散悬浮液滴团簇燃烧特性的影响

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摘要

For bridging between knowledge on droplet combustion and spray combustion, an experimental study was performed on autoignition and combustion of multiple droplet clusters. The monodispersed suspended-droplet cluster (MSDC) model with which arrangement, spacing and initial diameter of the droplet are well controlled has been developed. The effects of spacing and arrangement of droplet on combustion characteristics of the MSDC model in a high-temperature air were examined using microgravity environment in a drop shaft. The ignition delay and the burning time increased with decreasing the droplet spacing, regardless of the droplet number and the model dimensions. Larger droplet number with three-dimensional (3D) hexagonal closest packing (HCP) structure model resulted in longer ignition delay and longer burning time. 3D cubic closest packing (CCP) structure model showed rather longer ignition delay and much shorter burning time than 2D model. For 3D HCP model, an individual flame which enveloped each droplet was formed whole in the combustion duration with larger droplet spacing, while the group flame was formed whole in the combustion duration with smaller droplet spacing. When the droplet spacing was in the intermediate range, each droplet was ignited to form the individual flame, and each flame merged into the group flame. The diameter of the burning sphere decreased at the beginning of combustion, and turned to increase afterward. The transition from the individual flame to the group flame occurred around the time when the burning sphere diameter reached its minimum. The burning sphere diameter relative to the model diameter increased with decreasing the droplet spacing in the middle stage of combustion.
机译:为了在液滴燃烧和喷雾燃烧的知识之间架起桥梁,对多个液滴簇的自燃和燃烧进行了实验研究。已经开发出可以很好地控制液滴的排列,间距和初始直径的单分散悬浮液滴簇(MSDC)模型。使用微重力环境在滴井中检查了液滴的间距和排列对MSDC模型在高温空气中燃烧特性的影响。点火延迟和燃烧时间随液滴间距的减小而增加,而与液滴数量和模型尺寸无关。具有三维(3D)六边形最紧密堆积(HCP)结构模型的较大液滴数会导致更长的点火延迟和更长的燃烧时间。与2D模型相比,3D立方最紧密堆积(CCP)结构模型显示出更长的点火延迟和更短的燃烧时间。对于3D HCP模型,在整个燃烧持续时间内以较大的液滴间距形成单个火焰,该单个火焰包围每个液滴,而在燃烧持续时间内以较小的液滴间距形成整体火焰。当液滴间隔在中间范围内时,点燃每个液滴以形成单独的火焰,并且每个火焰合并成组火焰。燃烧球的直径在燃烧开始时就减小,然后又变大。从单个火焰到成组火焰的过渡发生在燃烧球直径达到最小值时。燃烧球直径相对于模型直径随着燃烧中间阶段液滴间距的减小而增加。

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