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Control-Volume Analysis Of Thrust-Augmenting EjectorsNew method of analysis of transient flow in thrust-augmenting ejector based on control-volume formulation of governing equations. Considered as potential elements of propulsion subsystems of short-takeoff/vertical-landing airplanes.
Document ID
19900000550
Document Type
Other - NASA Tech Brief
Authors
Drummond, Colin K. (Sverdrup Technology, Inc.)
Date Acquired
August 14, 2013
Publication Date
October 1, 1990
Publication Information
Publication: NASA Tech Briefs
Volume: 14
Issue: 10
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-14877
Accession Number
90B10550
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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