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Boundary-layer and Stalling Characteristics of the NACA 64A006 Airfoil Section
Document ID
19930082600
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mccullough, George B
Gault, Donald E
Date Acquired
August 16, 2013
Publication Date
August 1, 1949
Report/Patent Number
NACA-TN-1923
Report Number: NACA-TN-1923
Accession Number
93R11890
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL TESTS - AAL (10'X7',NO 1)
AIRFOILS - NACA 64A006 - CHAR & MOMENTS LOW-DRAG
PRESSURE DISTRIBUTION - AIRFOILS - NACA 64A006
BOUNDARY LAYER CONTROL - AIRFOILS - NACA 64A006
AIR FLOW - VISUALIZATION
AIR FLOW - AIRFOILS
STALLING
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