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Correlation of spray dropsize distribution and injector variablesThe 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.
Document ID
19720010642
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Zajac, L. J.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Subject Category
Fluid Mechanics
Report/Patent Number
R-7995
NASA-CR-125674
R-8455
Report Number: R-7995
Report Number: NASA-CR-125674
Report Number: R-8455
Accession Number
72N18292
Funding Number(s)
CONTRACT_GRANT: NAS7-726
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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