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An experimental study of multiple jet mixingMeasurements of an incompressible jet issuing from an array of rectangular lobes, equally spaced with their small dimensions in a line, both as a free jet, and as a confined jet, are carried out in three parts: (1) on a single rectangular free jet, (2) on the same jet in a multiple free jet configuration, and (3) on the same jet in a multiple jet configuration with confining surfaces (two parallel plates are symmetrically placed perpendicular to the long dimension of each lobe covering the entire flow field under consideration). In the case of a single rectangular free jet, the flow field of the jet is characterized by the presence of three distinct regions in the axial mean velocity decay and are referred to as: potential core region, two dimensional type region, and axisymmetric type region. In the case of a multiple free jet, the flow field for downstream distance X greater than 60D (D = width of a lobe) resembles that of a jet exiting from a two dimensional nozzle with its short dimension being the long dimension of the lobe.
Document ID
19800023253
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Krothapalli, D.
(Stanford Univ. CA, United States)
Baganoff, D.
(Stanford Univ. CA, United States)
Karamcheti, K.
(Stanford Univ. CA, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1979
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
SU-JIAA-TR-23
NASA-CR-166184
Report Number: SU-JIAA-TR-23
Report Number: NASA-CR-166184
Accession Number
80N31760
Funding Number(s)
CONTRACT_GRANT: NSG-2233
CONTRACT_GRANT: NSG-2007
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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