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Effects of Propellers and of Vibration on the Extent of Laminar Flow on the NACA 27-212 Airfoil
Document ID
19930092787
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gaydos, M Edward
Date Acquired
September 6, 2013
Publication Date
October 1, 1939
Report/Patent Number
NACA-WR-L-784
Report Number: NACA-WR-L-784
Accession Number
93R22077
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE DISTRIBUTION - AIRFOILS - NACA 27-212
BOUNDARY LAYER - AIRFOILS LAMINAR
WIND TUNNEL TESTS - NACA - HIGH-SPEED (8')
AIRFOILS - NACA 27-212 LAMINAR-FLOW
BOUNDARY LAYER TRANSITION
AIRFOILS - NACA - LAMINAR-FLOW

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