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Aerodynamic Tests of an NACA 66(215)-116, A=0.6 Airfoil With a 0.25c Slotted Flap for the Fleetwings XA-39 Airplane
Document ID
19930092801
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Cahill, Jones F
Date Acquired
September 6, 2013
Publication Date
November 1, 1944
Report/Patent Number
NACA-MR-L4K21
NACA-WR-L-629
Report Number: NACA-MR-L4K21
Report Number: NACA-WR-L-629
Accession Number
93R22091
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOW-DRAG (WING FLAPS, SLOTTED)
WING FLAPS, SLOTTED
WINGS-FLEETWINGS A-39-WIND TUNNEL TESTS-(NACA-LOW-TURBULENCE & PRESSURE, LOW TUR
AIRFOILS - NACA 66(215)-116 - CHAR , MOMENTS & ORDINATES

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