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NASA NTRS · 19830054828

Entrainment and mixing in thrust augmenting ejectors

Abstract

An experimental investigation of two-dimensional thrust augmenting ejector flows has been conducted. Measurements of the shroud surface pressure distribution, mean velocity, turbulent intensities and Reynolds stresses were made in two shroud geometries at various primary nozzle pressure ratios. The effects of shroud geometry and primary nozzle pressure ratio on the shroud surface pressure distribution, mean flow field and turbulent field were determined. From these measurements the evolution of mixing within the shroud of the primary flow and entrained fluid was obtained. The relationship between the mean flow field, the turbulent field and the shroud surface pressure distribution is discussed.

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BibTeXRIS

Bernal, L., Sarohia, V.. 1983-01-01. Entrainment and mixing in thrust augmenting ejectors. https://ntrs.nasa.gov/citations/19830054828

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