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An experimental investigation of the NACA 631-012 airfoil section with leading-edge and midchord suction slots
Document ID
19930082697
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mccullough, George B
Gault, Donald E
Date Acquired
August 16, 2013
Publication Date
February 1, 1950
Report/Patent Number
NACA-TN-2041
Report Number: NACA-TN-2041
Accession Number
93R11987
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - NACA 631-012 - CHAR & MOMENTS - LOW-DRAG
WIND TUNNEL TESTS - AAL (10'X7')
BOUNDARY LAYER CONTROL - AIRFOILS - NACA 631-012
BOUNDARY LAYER CONTROL - SUCTION - SLOTS
PRESSURE DISTRIBUTION - AIRFOILS - NACA 631-012

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