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Recent developments in ejector technology in the Air Force: An overviewBasic and applied studies in thrust augmentation conducted at the Aerospace Research Laboratory at Wright-Patterson AFB which led to an effective configuration of the jet flap diffuser ejector, are reviewed. A method for compressible ejector flow analysis, developed in support of the preliminary design of an ejector thrust aircraft, is discussed and applied to single- and two-stage ejectors.
Document ID
19800001869
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nagaraja, K. S. (Air Force Flight Dynamics Lab. Wright-Patterson AFB, OH, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1979
Publication Information
Publication: NASA. Ames Res. Center Workshop on Thrust Augmenting Ejectors
Subject Category
Aerodynamics
Accession Number
80N10108
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19800001868Collected WorksWorkshop on Thrust Augmenting Ejectors
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