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Low-speed wind-tunnel studies relating to pitch-up on a supersonic transport model with a high-aspect-ratio variable-sweep wingLow speed wind tunnel testing of high aspect ratio variable sweep wing supersonic transport model for determining methods of reducing pitch-up tendency
Document ID
19660023730
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Lockwood, V. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-3542
Report Number: NASA-TN-D-3542
Accession Number
66N33020
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PITCH CONTROL
SUPERSONIC TRANSPORT
ASPECT RATIO
SWEPT WING
WIND TUNNEL MODEL

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