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Full-scale wind-tunnel investigation of a VTOL aircraft with a jet-ejector system for lift augmentationFull scale wind tunnel investigation of VTOL AIRCRAFT with jet ejector system for lift augmentation
Document ID
19670022992
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hickey, D. H. (NASA Ames Research Center Moffett Field, CA, United States)
Kirk, J. V. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1966
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-3725
Report Number: NASA-TN-D-3725
Accession Number
67N32321
Funding Number(s)
CONTRACT_GRANT: 721-01-00-08-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
WIND TUNNEL STABILITY TEST
VTOL AIRCRAFT
LIFT AUGMENTATION
EJECTOR

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