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NASA NTRS · 19810021591

Entrainment and thrust augmentation in pulsatile ejector flows

Abstract

This study comprised direct thrust measurements, flow visualization by use of a spark shadowgraph technique, and mean and fluctuating velocity measurements with a pitot tube and linearized constant temperature hot-wire anemometry respectively. A gain in thrust of as much as 10 to 15% was observed for the pulsatile ejector flow as compared to the steady flow configuration. From the velocity profile measurements, it is concluded that this enhanced augmentation for pulsatile flow as compared to a nonpulsatile one was accomplished by a corresponding increased entrainment by the primary jet flow. It is also concluded that the augmentation and total entrainment by a constant area ejector critically depends upon the inlet geometry of the ejector. Experiments were performed to evaluate the influence of primary jet to ejector area ratio, ejector length, and presence of a diffuser on pulsatile ejector performance.

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BibTeXRIS

Sarohia, V., Bernal, L., Bui, T.. 1981-08-15. Entrainment and thrust augmentation in pulsatile ejector flows. https://ntrs.nasa.gov/citations/19810021591

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