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NASA overviewThe history of NASA efforts at Ames Research Center in researching the performance and application of thrusting augmentors is reviewed. Current objectives include: (1) parametric description of thrust augmentor application to STOL and V/STOL; (2) the use of theoretical and empirical data; (3) aircraft-augmentor integration; and (4) key design considerations for STOL transport and V/STOL fighter aircraft. Test facilities are described and ejector development and performance are assessed.
Document ID
19800001870
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Koenig, D. G. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1979
Publication Information
Publication: Workshop on Thrust Augmenting Ejectors
Subject Category
Aerodynamics
Accession Number
80N10109
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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