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Lift and Drag Tests of Three Airfoil Models with Fowler Flaps Submitted by Consolidated Aircraft Corporation
Document ID
19930092770
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Turner, Harold R , Jr
Date Acquired
September 6, 2013
Publication Date
December 1, 1941
Report/Patent Number
NACA-WR-L-677
Report Number: NACA-WR-L-677
Accession Number
93R22060
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING FLAPS - FOWLER
AIRFOILS - DAVIS - CHARACTERISTICS - LAMINAR-FLOW (WING FLAPS, FOWLER )
WING FLAPS - DEFLECTION
WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE (7 1/2' X 3')
AIRFOILS, GLOVE
LOW-DRAG (WING FLAPS, FOWLER)
WINGS CONSOLIDATED B-32 WIND TUNNEL TESTS (NACA - 2-DIM PRESSURE)
AIRFOILS - NACA 65,2-221 - 66,2X-416 - CHAR

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