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Wind-tunnel Investigation of Split Trailing-edge Lift and Trim Flaps on a Tapered Wing with 23 Degree Sweepback
Document ID
19930081977
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Letko, William
Feigenbaum, David
Date Acquired
August 16, 2013
Publication Date
July 1, 1947
Report/Patent Number
NACA-TN-1352
Report Number: NACA-TN-1352
Accession Number
93R11267
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING FLAPS, TRIM
AIRFOILS - NACA 4418 - CHAR , MOMENTS & ORDINATES WING FLAPS
SPLIT
WINGS, TAPERED - CHARACTERISTICS
PRESSURE DISTRIBUTION - AIRFOILS - NACA 4418
WINGS, SWEPTBACK
WINGS, SWEPTBACK - STABILITY
EFFECT OF WING FLAPS
WIND TUNNEL TESTS - NACA - STABILITY
WING FLAPS - DEFLECTION

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