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Analysis of available data on the effectiveness of ailerons without exposed overhang balance
Document ID
19930092936
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Crandall, Stewart M.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Swanson, Robert S.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1944
Report/Patent Number
NACA-WR-L-171
NACA-ACR-L4E01
Report Number: NACA-WR-L-171
Report Number: NACA-ACR-L4E01
Accession Number
93R22226
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LATERAL CONTROL
THEORIES - AIRFOILS - LIFTING-LINE
AIRFOILS - NACA - LOW-DRAG
AILERONS - EFFICIENCY
AILERONS, SEALED-GAP
ROLLING MOMENTS - AILERONS
WING FLAPS - DEFLECTION
AILERONS - DEFLECTION
WING FLAPS, BALANCED - INTERNAL
AILERONS, BALANCED - OVERHANG
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