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Coaxial airblast atomizersAn experimental investigation was performed to quantify the characteristics of the sprays of coaxial injectors with particular emphasis on those aspects relevant to the performance of rocket engines. Measurements for coaxial air blast atomizers were obtained using air to represent the gaseous stream and water to represent the liquid stream. A wide range of flow conditions were examined for sprays with and without swirl for gaseous streams. The parameters varied include Weber number, gas flow rate, liquid flow rate, swirl, and nozzle geometry. Measurements were made with a phase Doppler velocimeter. Major conclusions of the study focused upon droplet size as a function of Weber number, effect of gas flow rate on atomization and spray spread, effect of nozzle geometry on atomization and spread, effect of swirl on atomization, spread, jet recirculation and breakup, and secondary atomization.
Document ID
19940010636
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hardalupas, Y.
(Imperial Coll. of Science and Technology London, United Kingdom)
Whitelaw, J. H.
(Imperial Coll. of Science and Technology London, United Kingdom)
Date Acquired
September 6, 2013
Publication Date
May 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
SRA-R93-9083-F
NASA-CR-193845
NAS 1.26:193845
Report Number: SRA-R93-9083-F
Report Number: NASA-CR-193845
Report Number: NAS 1.26:193845
Accession Number
94N15109
Funding Number(s)
CONTRACT_GRANT: NAS8-38872
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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