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Near-field Film Thickness Measurements of an LPRE Swirl Injector Spray

机译:LPRE旋流喷射器喷雾的近场膜厚测量

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A novel approach to the measure of liquid film thickness in the near-field of a liquid rocket swirl injector spray was developed. Archived data were analyzed, wherein liquid mass flow was throttled over a range of 0.064 to 0.082 kg/s-corresponding to injection pressure drops of 0.80 to 1.26 MPa. For these conditions, digital images of the swirling liquid sheet were deconvoluted with an Abel transform technique and processed with an objective film thickness measurement algorithm. Measurements were benchmarked against theoretical values of the injection film thickness, as well as empirical predictions of film thickness at the injection plane and slightly upstream within the injector nozzle. Results suggest this approach successfully discerns film thickness; however, uncertainties associated with the measurements limit definitive physical insight on film thickness behavior as a function of the particular test conditions presented in this work.
机译:提出了一种测量液体火箭旋流喷射器近场中液膜厚度的新方法。分析存档的数据,其中液体质量流量在0.064至0.082 kg / s的范围内节流,对应于0.80至1.26 MPa的喷射压降。在这些条件下,用Abel变换技术对旋涡状液体片的数字图像进行反卷积,并用客观的膜厚测量算法进行处理。相对于喷射膜厚度的理论值以及在喷射平面和喷射器喷嘴内稍上游的膜厚度的经验预测,对测量进行基准测试。结果表明该方法成功地识别了膜的厚度。然而,与测量相关的不确定性限制了对薄膜厚度行为的确切物理洞察力,这是这项工作中提出的特定测试条件的函数。

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