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Tests of the NACA 64(SUB 1)A212 Airfoil Section with a Slat, a Double Slotted Flap, and Boundary-layer Control by Suction
Document ID
19930081912
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Quinn, John H
Date Acquired
August 16, 2013
Publication Date
May 1, 1947
Report/Patent Number
NACA-TN-1293
Report Number: NACA-TN-1293
Accession Number
93R11202
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SLOTTED (DOUBLE))
WING FLAPS, SLOTTED - DOUBLE
WINGS - HIGH LIFT DEVICES
REYNOLDS NUMBER
BOUNDARY LAYER CONTROL - SUCTION-SLOTS
AIRFOILS - NACA 641A212 - CHAR & ORDINATES LOW-DRAG (WING FLAPS,
WIND TUNNEL TESTS - NACA - LOW-TURBULENCE (7 1/2'X 3') WORK CARRIED ON AT LMAL
AIRFOIL SURFACES - ROUGHNESS
WING SLATS

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