Fig. 9 | Scientific Reports

Fig. 9

From: Experimental study on the change of the orientation of high aspect ratio nozzle slit relative to the airflow

Fig. 9

Flow structure of the two-dimensional liquid sheet at \(\theta \) = 90 and constant momentum ratio of 100, (a)\({We}_{s}\) = 4.86, \({We}_{g}\) = 0.05, q = 100, (b) \({We}_{s}\) = 12.44, \({We}_{g}\) = 0.12, (c) \({We}_{s}\) = 19.4, \({We}_{g}\) = 0.19, (d) \({We}_{s}\) = 32.8, \({We}_{g}\) = 0.33, (e) \({We}_{s}\) = 49.8, \({We}_{g}\) = 0.5.

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