NASA NTRS ยท 19720010642
Correlation of spray dropsize distribution and injector variables
Abstract
The atomization characteristics of impinging stream rocket engine injection elements are studied to determine the effects of hydraulic and geometric parameters on the mass median drop size. The major conclusions are: (1) the velocity profile of impinging jets affects mean drop size, this effect is greater when the jets are laminar than when they are turbulent; (2) the drop size/injection velocity dependence for turbulent jet impingement differs from that obtained with non-turbulent jets; (3) the level of turbulence intensity does not affect mean drop size; (4) the impingement of disintegrated or nearly disintegrated jets substantially decreases atomization; and (5) even though an emulsion is formed when immiscible jets impinge, the level of emulsification is small.
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Zajac, L. J.. 1971-01-01. Correlation of spray dropsize distribution and injector variables. https://ntrs.nasa.gov/citations/19720010642
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