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Cryogenic spray vaporization in high-velocity helium, argon and nitrogen gasflows

机译:高速氦,氩和氮气流中的低温喷雾蒸发

摘要

Effects of gas properties on cryogenic liquid-jet atomization in high-velocity helium, nitrogen, and argon gas flows were investigated. Volume median diameter, D(sub v.5e), data were obtained with a scattered-light scanning instrument. By calculating the change in spray drop size, -Delta D(sub v.5)(exp 2), due to droplet vaporization, it was possible to calculate D(sub v.5C). D(sub v.5C) is the unvaporized characteristic drop size formed at the fuel-nozzle orifice. This drop size was normalized with respect to liquid-jet diameter, D(sub O). It was then correlated with several dimensionless groups to give an expression for the volume median diameter of cryogenic LN2 sprays. This expression correlates drop size D(sub v.5c) with aerodynamic and liquid-surface forces so that it can be readily determined in the design of multiphase-flow propellant injectors for rocket combustors.
机译:研究了气体特性对高速氦,氮和氩气流中低温液体喷射雾化的影响。体积中值直径D(sub v.5e)数据是使用散射光扫描仪获得的。通过计算由于液滴汽化而引起的液滴尺寸变化-ΔD(sub v.5)(exp 2),可以计算D(sub v.5C)。 D(sub v.5C)是在燃料喷嘴孔口处形成的未蒸发的特征液滴尺寸。相对于液体喷射直径D(sub O)将液滴尺寸标准化。然后将其与几个无量纲的组相关联,以表示低温LN2喷雾的体积中值直径。该表达式将液滴尺寸D(sub v.5c)与空气动力和液体表面力相关联,因此可以在火箭燃烧器的多相流推进剂喷射器设计中轻松确定它。

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  • 作者

    Ingebo Robert D.;

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  • 年度 1993
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