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Wind-Tunnel Investigation of Aileron Effectiveness of 0.20-Airfoil-Chord Plain Ailerons of True Airfoil Contour on NACA 65(sub 2)-415, 65(sub 3)-418 and 65(sub 4)-421 Airfoil Sections
Document ID
19930092788
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Braslow, Albert L
Date Acquired
September 6, 2013
Publication Date
August 1, 1944
Report/Patent Number
NACA-CB-L4H12
NACA-WR-L-178
Report Number: NACA-CB-L4H12
Report Number: NACA-WR-L-178
Accession Number
93R22078
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS-NACA 653-418-CHAR & ORDINATES LOW-DRAG
WIND TUNNEL TESTS-NACA-PRESSURE, TWO-DIMENSIONAL (7 1/2' X 3')
AIRFOILS-NACA 652-415-CHAR & ORDINATES LOW-DRAG
AILERONS - EFFICIENCY
AILERONS - DEFLECTION
AILERONS, SEALED-GAP
AIRFOILS-NACA 654-421-CHAR & ORDINATES LOW-DRAG

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