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NASA NTRS · 19940028363

Shear flow control of cold and heated rectangular jets by mechanical tabs. Volume 2: Tabulated data

Abstract

The 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.

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Brown, W. H., Ahuja, K. K.. 1989-05-01. Shear flow control of cold and heated rectangular jets by mechanical tabs. Volume 2: Tabulated data. https://ntrs.nasa.gov/citations/19940028363

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