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The external augmentor concept for V/STOL aircraftThe beneficial aspects of an ejector powered V/STOL concept were reviewed. The feasibility of satisfactorily incorporating an ejector system in a high performance V/STOL aircraft was investigated. The external augmentor concept, based on the use of chordwise ejector slots, is presented. It is concluded that the external augmentor concept has a basic inherent simplicity and a sufficient augmentor performance potential to make feasible a high performance V/STOL aircraft based on ejectors.
Document ID
19800001893
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Whittely, D. C. (De Havilland Aircraft Co. of Canada Ltd. Ottawa Ontario, Canada)
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
80N10132
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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