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LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT LOW SUBSONIC SPEEDS OF A HIGHLY SWEPT DELTA WING UTILIZING NOSE DEFLECTION FOR CONTROLLongitudinal aerodynamic characteristics at low subsonic speeds of a highly swept delta wing with nose deflection control
Document ID
19630000325
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Spencer, B., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1962
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TN-D-1482
Report Number: NASA-TN-D-1482
Accession Number
63N10199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SWEPT WING
SUBSONIC SPEED
AERODYNAMIC CHARACTERISTICS
DELTA WING

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