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
Joint Propulsion Conference ; 1989 ; Monterey, CA, United States
01.01.1989
Aufsatz (Konferenz)
Keine Angabe
Englisch
AIAA | 2010
|