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Droplet breakup in accelerating gas flows. Part 2: Secondary atomizationAn experimental investigation to determine the effects of an accelerating gas flow on the atomization characteristics of liquid sprays was conducted. The sprays were produced by impinging two liquid jets. The liquid was molten wax and the gas was nitrogen. The use of molten wax allowed for a quantitative measure of the resulting dropsize distribution. The results of this study, indicate that a significant amount of droplet breakup will occur as a result of the action of the gas on the liquid droplets. Empirical correlations are presented in terms of parameters that were found to affect the mass median dropsize most significantly, the orifice diameter, the liquid injection velocity, and the maximum gas velocity. An empirical correlation for the normalized dropsize distribution is also presented. These correlations are in a form that may be incorporated readily into existing combustion model computer codes for the purpose of calculating rocket engine combustion performance.
Document ID
19730022516
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Zajac, L. J.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1973
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-134479
R-9337-2-PT-2
Report Number: NASA-CR-134479
Report Number: R-9337-2-PT-2
Accession Number
73N31248
Funding Number(s)
CONTRACT_GRANT: NAS3-14371
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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