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Aerodynamic Characteristics of a Spoiler-Slot-Deflector Control on a 45 deg Sweptback-Wing-Fuselage Model at High Subsonic SpeedsLateral control & hinge moment of spoiler-slot- deflector on sweptback wing at subsonic speed
Document ID
19640000708
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hammond, A. D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-2037
Report Number: NASA-TN-D-2037
Accession Number
64N10617
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HINGE MOMENT
LATERAL CONTROL
SUBSONIC SPEED
SWEPTBACK WING
SPOILER-SLOT AILERON

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