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Boundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel
Document ID
19930092775
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Wartime Report
Authors
Becker, John V
Date Acquired
September 6, 2013
Publication Date
January 1, 1940
Report/Patent Number
NACA-WR-L-682
Report Number: NACA-WR-L-682
Accession Number
93R22065
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL TESTS - NACA - HIGH-SPEED (8')
PRESSURE DISTRIBUTION - AIRFOILS - NACA 0012
PRESSURE DISTRIBUTION - AIRFOILS - NACA 23012
BOUNDARY LAYER TRANSITION - WINGS
SKIN FRICTION - AIRFOILS
AIRFOILS - NACA 23012 - CHARACTERISTICS
AIRFOILS - NACA 0012 - CHARACTERISTICS

Related Records

IDRelationTitle20090014208See AlsoBoundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel, Special Report
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