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Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured in Flight on the Wing of the D-558-I Research Airplane Through a Mach Number Range of 0.80 to 0.89 and Throughout the Normal-force-coefficient Range at Mach Numbers of 0.61, 0.7
Document ID
19930086693
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Keener, Earl R
Bandish, Rozalia M
NACA
Date Acquired
August 16, 2013
Publication Date
August 20, 1951
Report/Patent Number
NACA-RM-L51F12
Report Number: NACA-RM-L51F12
Accession Number
93R15983
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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