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Effect of skewed wing-tip controls on a variable-sweep wing-fuselage configurationSkewed wing tip control effects on variable sweep wing-fuselage configuration
Document ID
19670009634
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Grow, J. W. (NASA Langley Research Center Hampton, VA, United States)
Landrum, E. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-3847
Report Number: NASA-TN-D-3847
Accession Number
67N18963
Funding Number(s)
CONTRACT_GRANT: 126-13-02-04-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING TIP CONTROL
VARIABLE SWEEP
WING-FUSELAGE COMBINATION

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