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Some Effects of Reynolds and Mach Numbers on the Lift of an NACA 0012 Rectangular Wing in the NACA 19-Foot Pressure Tunnel
Document ID
19930092735
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Muse, Thomas C
Date Acquired
September 6, 2013
Publication Date
May 1, 1943
Report/Patent Number
NACA-CB-3E29
NACA-WR-L-406
Report Number: NACA-CB-3E29
Report Number: NACA-WR-L-406
Accession Number
93R22025
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MACH NUMBER
LIFT COEFFICIENTS - AIRFOILS - NACA 0012
REYNOLDS NUMBER
WINGS, RECTANGULAR - CHARACTERISTICS
WIND TUNNEL TESTS - NACA - PRESSURE (19')
AIR FLOW - COMPRESSIBILITY

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