NASA NTRS · 19890062317
Transient flow thrust prediction for an ejector propulsion concept
Abstract
A method for predicting transient thrust augmenting ejector characteristics is introduced. The analysis blends classic self-similar turbulent jet descriptions with a mixing region control volume analysis to predict transient effects in a new way. Details of the theoretical foundation, the solution algorithm, and sample calculations are given.
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Drummond, C.. 1989-07-01. Transient flow thrust prediction for an ejector propulsion concept. https://ntrs.nasa.gov/citations/19890062317
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