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Shear flow control of cold and heated rectangular jets by mechanical tabs. Volume 2: Tabulated dataThe effects of mechanical protrusions on the jet mixing characteristics of rectangular nozzles for heated and unheated subsonic and supersonic jet plumes were studied. The characteristics of a rectangular nozzle of aspect ratio 4 without the mechanical protrusions were first investigated. Intrusive probes were used to make the flow measurements. Possible errors introduced by intrusive probes in making shear flow measurements were also examined. Several scaled sizes of mechanical tabs were then tested, configured around the perimeter of the rectangular jet. Both the number and the location of the tabs were varied. From this, the best configuration was selected. This volume contains tabulated data for each of the data runs cited in Volume 1. Baseline characteristics, mixing modifications (subsonic and supersonic, heated and unheated) and miscellaneous charts are included.
Document ID
19940028363
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brown, W. H.
(Lockheed Aeronautical Systems Co. Marietta, GA, United States)
Ahuja, K. K.
(Lockheed Aeronautical Systems Co. Marietta, GA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
LG89ER0059-VOL-2
NASA-CR-182296-VOL-2
NAS 1.26:182296-VOL-2
Report Number: LG89ER0059-VOL-2
Report Number: NASA-CR-182296-VOL-2
Report Number: NAS 1.26:182296-VOL-2
Accession Number
94N32869
Funding Number(s)
CONTRACT_GRANT: NAS3-25409
PROJECT: RTOP 505-62-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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