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Flow structure within a heated rectangular jet ejectorPreliminary results of an experimental study of the flow field structure within a rectangular jet ejector are presented. The tests determined the effect of primary jet heating and ejector duct width on the flow field at a fixed jet exit Mach number of 0.3. For comparison the rectangular jet without the presence of the ejector shroud was also studied. Measurements of the mean velocity field, total temperature field, and ejector shroud surface pressure distribution, along with schlieren flow visualization, were made. It was found that: the ejector did not enhance centerline temperature decay in comparison to the free jet; the presence of the ejector shroud significantly reduced jet growth; and, the ejector centerline velocity/temperature decay was not sensitive to duct width variations.
Document ID
19840036480
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mclachlan, B. G.
(NASA Ames Research Center Moffett Field; Stanford University, Stanford, CA, United States)
Krothapalli, A.
(Florida State University Tallahassee, FL, United States)
Nagaraja, K.
(USAF, Wright Aeronautical Laboratories, Wright-Patterson AFB OH, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 84-0571
Report Number: AIAA PAPER 84-0571
Accession Number
84A19267
Distribution Limits
Public
Copyright
Other

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