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Comparison of experimental and numerical investigation on a jet in a supersonic cross-flow

机译:超声速横流中射流的实验与数值研究比较

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摘要

Flow interaction of three different jet configurations ejecting air from a flat plate into a supersonic cross flow were investigated experimentally and numerically. The test conditions encompassed a jet pressure ratio of P_(0j), P_∞ = 100 at a Mach number of M_∞ = 5 and Reynolds number of about Re_∞ = 25 x 10~6 based on the length of the flat plate. The investigated test cases are: a) single jet; b) four jets positioned in-line in main flow direction; c) four jets positioned side-by-side in spanwise direction. The prediction of the overall flow phenomena as occurring within the interaction area was in fair agreement with the experiments, although quantitatively differences occur that will be discussed in the paper. The results of the comparison are presented and the experimental data are used to validate the applied code.
机译:实验和数值研究了三种不同的射流形态将空气从平板喷射到超声速横流中的流动相互作用。测试条件包括基于平板长度的马赫数M_∞= 5时的射流压力比P_(0j),P_∞= 100和雷诺数约为Re_∞= 25 x 10〜6。调查的测试案例是:a)单喷射; b)在主流方向成一直线排列的四个喷嘴; c)在翼展方向上并排放置的四个喷嘴。尽管发生了定量差异,但对相互作用区域内整体流动现象的预测与实验基本吻合。给出了比较结果,并使用实验数据验证了所应用的代码。

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