NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Experiments in dilution jet mixing - Effects of multiple rows and non-circular orificesExperimental and empirical model results are presented that extend previous studies of the mixing of single-sided and opposed rows of jets in a confined duct flow to include effects of non-circular orifices and double rows of jets. Analysis of the mean temperature data obtained in this investigation showed that the effects of orifice shape and double rows are significant only in the region close to the injection plane, provided that the orifices are symmetric with respect to the main flow direction. The penetration and mixing of jets from 45-degree slanted slots is slightly less than that from equivalent-area symmetric orifices. The penetration from two-dimensional slots is similar to that from equivalent-area closely-spaced rows of holes, but the mixing is slower for the 2-D slots. Calculated mean temperature profiles downstream of jets from non-circular and double rows of orifices, made using an extension developed for a previous empirical model, are shown to be in good agreement with the measured distributions.
Document ID
19850057455
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Holdeman, J. D.
(NASA Lewis Research Center Modeling and Verification Branch, Cleveland, OH, United States)
Srinivasan, R.
(NASA Lewis Research Center Cleveland, OH, United States)
Coleman, E. B.
(NASA Lewis Research Center Cleveland, OH, United States)
Meyers, G. D.
(NASA Lewis Research Center Cleveland, OH, United States)
White, C. D.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Date Acquired
August 12, 2013
Publication Date
July 1, 1985
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 85-1104
Accession Number
85A39606
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available