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Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modifications of aileron nose and adjacent airfoil contour
Document ID
19930092934
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bird, J D
Date Acquired
September 6, 2013
Publication Date
February 1, 1945
Report/Patent Number
NACA-WR-L-105
NACA-ACR-L5B10
Report Number: NACA-WR-L-105
Report Number: NACA-ACR-L5B10
Accession Number
93R22224
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AILERONS, BEVELED
WIND TUNNEL TESTS - NACA - STABILITY
AILERONS - NOSE-SHAPE
AIRFOILS - NACA 55(215)-216-ORDINATES
AILERONS, BALANCED - SEALED-GAP
AILERONS, BALANCED - OVERHANG
AILERONS, BALANCED - HINGE MOMENTS

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