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Combustion Visualization of Paraffin-Based Hybrid Rocket Fuel at Elevated Pressures

机译:石蜡基混合火箭燃料在高压下的燃烧可视化

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The discovery of high regression rate liquefying fuels for hybrid motors has generated a renewed interest in visualization experiments. In 2012, the Stanford Combustion Visualization Facility was developed to investigate the combustion of these fuels with gaseous oxygen. A major upgrade of this facility was recently completed. Details of the changes made to the facility are provided. Visual and schlieren images of the combustion of paraffin wax and oxygen at a range of operating pressures are presented, including the first schlieren images of the combustion of paraffin wax and oxygen at supercritical pressures. The nature of the combustion and the boundary layer thickness were seen to change dramatically with increasing chamber pressure, up to approximately the critical pressure of the fuel. Droplet entrainment from the surface of the fuel grain was observed at all pressures. At elevated pressures the combustion of the fuel grain was characterized by very strong surface blowing events comprised of numerous droplets.
机译:用于混合动力发动机的高回归速率液化燃料的发现引起了对可视化实验的新兴趣。 2012年,斯坦福大学燃烧可视化设施被开发出来,以研究这些燃料与气态氧的燃烧。最近完成了对该设施的重大升级。提供了对设施所做的更改的详细信息。给出了在一定工作压力下石蜡和氧气燃烧的视觉和席勒图像,包括在超临界压力下石蜡和氧气燃烧的第一席勒图像。燃烧的性质和边界层的厚度随腔室压力的增加而急剧变化,直至接近燃料的临界压力。在所有压力下均观察到从燃料颗粒表面的液滴夹带。在升高的压力下,燃料颗粒的燃烧的特征在于非常强烈的表面吹扫事件,该事件由许多液滴组成。

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