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Wind-tunnel Investigation at Low Speed of the Lateral Control Characteristics of an Unswept Untapered Semi-span Wing of Aspect Ratio 3.13 Equipped with Various 25-percent-chord Plain Ailerons
Document ID
19930082848
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Johnson, Harold S
Hagerman, John R
Date Acquired
August 16, 2013
Publication Date
October 1, 1950
Report/Patent Number
NACA-TN-2199
Report Number: NACA-TN-2199
Accession Number
93R12138
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AILERONS - POSITION
AILERONS - HINGE MOMENTS
ROLLING, PITCHING & YAWING MOMENTS - WINGS
AILERON CONTROLS
AILERONS - DEFLECTION
AIRFOILS - NACA 64A010
WINGS - CHARACTERISTICS
WIND TUNNEL TESTS - NACA - 300 MPH (10 FEET X 7 FEET)

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