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Multiple jet studyTest data is presented which allows determination of jet penetration and mixing of multiple cold air jets into a ducted subsonic heated mainstream flow. Jet-to-mainstream momentum flux ratios ranged from 6 to 60. Temperature profile data is presented at various duct locations up to 24 orifice diameters downstream of the plane of jet injection. Except for two configurations, all geometries investigated had a single row of constant diameter orifices located transverse to the main flow direction. Orifice size and spacing between orifices were varied. Both of these were found to have a significant effect on jet penetration and mixing. The best mixing of the hot and cold streams was achieved with duct height.
Document ID
19730017559
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Walker, R. E.
(Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Kors, D. L.
(Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1973
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-121217
Report Number: NASA-CR-121217
Accession Number
73N26286
Funding Number(s)
CONTRACT_GRANT: NAS3-15703
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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