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Test of NACA 66,2-116, a = 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane
Document ID
19930092767
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Abbott, Frank T , Jr
Date Acquired
September 6, 2013
Publication Date
May 1, 1942
Report/Patent Number
NACA-WR-L-701
Report Number: NACA-WR-L-701
Accession Number
93R22057
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING FLAPS, SLOTTED
WING FLAPS, BALANCED
PRESSURE DISTRIBUTION - WING FLAPS
AIRFOILS - NACA 66,2-116 - CHAR & MOMENTS LOW-DRAG (WING FLAPS, BALANCED & SLOT
WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE (7 1/2' X 3')
WINGS - BELL P-63 WIND TUNNEL TESTS (NACA - 2-DIM PRESSURE)
WING FLAPS - HINGE MOMENTS

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