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The Effects of Mach Number and Reynolds Number on the Aerodynamic Characteristics of Several 12-percent-thick Wings Having 35 Degrees of Sweepback and Various Amounts of Camber
Document ID
19930086568
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Tinling, Bruce E
Kolk, W Richard
Date Acquired
August 16, 2013
Publication Date
February 23, 1951
Report/Patent Number
NACA-RM-A50K27
Report Number: NACA-RM-A50K27
Accession Number
93R15858
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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