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.
Transient flow thrust prediction for an ejector propulsion concept
01.07.1989
Aufsatz (Konferenz)
Keine Angabe
Englisch
AIAA | 2010
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