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Two-dimensional Wind-tunnel Investigation of Spoiler Aileron Flap Model for the Hughes XF-11 Airplane
Document ID
19930092940
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Fullmer, Felicien F , Jr
Date Acquired
September 6, 2013
Publication Date
April 1, 1945
Report/Patent Number
NACA-MR-L5C29
NACA-WR-L-644
Accession Number
93R22230
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING SPOILERS, RETRACTABLE
AILERONS, RETRACTABLE
WING FLAPS, SLOTTED & AILERONS, RETRACTABLE
WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE (7 1/2' X 3')
AIRFOILS - NACA 66(215)-216 (APPROX ) - CHAR , MOMENTS & ORDINATES
LOW-DRAG (WING FLAPS, SLOTTED)
WIND TUNNEL TESTS - NACA - LOW-TURBULENCE (7 1/2' X 3')
AILERONS - HUGHES F-11

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