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Large-scale wind-tunnel tests of an airplane model with an unswept tilt wing of aspect ratio of 5.5, and with various stall control devicesWind-tunnel stability tests of tilt-wing vtol aircraft
Document ID
19640004814
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Giulianetti, D. J. (NASA Ames Research Center Moffett Field, CA, United States)
Weiberg, J. A. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1964
Subject Category
Biosciences
Report/Patent Number
NASA-TN-D-2133
Report Number: NASA-TN-D-2133
Accession Number
64N14728
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL STABILITY TEST
VTOL AIRCRAFT

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