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NASA NTRS · 19840036480

Flow structure within a heated rectangular jet ejector

Abstract

Preliminary 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.

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BibTeXRIS

Mclachlan, B. G., Krothapalli, A., Nagaraja, K.. 1984-01-01. Flow structure within a heated rectangular jet ejector. https://ntrs.nasa.gov/citations/19840036480

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