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Tabulated pressure coefficients and aerodynamic characteristics measured in flight on the wing of the Douglas D-558-I airplane for a 1 g stall, a speed run to a Mach number of 0.90, and a wind-up turn at a Mach number of 0.86
Document ID
19930086579
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Keener, Earl R
Pierce, Mary
Date Acquired
August 29, 2013
Publication Date
December 1, 1950
Report/Patent Number
NACA-RM-L50J10
Accession Number
93R15869
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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