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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
19650068445
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Keener, E. R. (NASA Langley Research Center Hampton, VA, United States)
Pierce, M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 2, 2013
Publication Date
December 15, 1950
Subject Category
Unknown
Report/Patent Number
NACA-RM-L50J10
Report Number: NACA-RM-L50J10
Accession Number
65N80846
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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