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Wind-tunnel Investigation of the NACA 654-421 Airfoil Section with a Double Slotted Flap and Boundary Layer Control by Suction
Document ID
19930082039
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Quinn, John H
Date Acquired
August 16, 2013
Publication Date
July 1, 1947
Report/Patent Number
NACA-TN-1395
Report Number: NACA-TN-1395
Accession Number
93R11329
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL TESTS - NACA - LOW-TURBULENCE (7 1/2'X 3') WORK CARRIED ON AT LMAL
WING FLAPS, SLOTTED - DOUBLE
BOUNDARY LAYER CONTROL - AIRFOILS - NACA 654-421
AIRFOILS - CHARACTERISTICS EFFECT OF SURFACE ROUGHNESS
SLOTTED (DOUBLE))
BOUNDARY LAYER CONTROL - SUCTION - SLOTS
AIRFOILS - NACA 654-421 - CHAR & ORDINATES LOW-DRAG(WING FLAPS,

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