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The Effect of Sweepback on the Longitudinal Characteristics at a Mach Number of 1.24 of a 1/30 Scale Semispan Model of the Bell X-5 Airplane from Tests by the NACA Wing Flow Method
Document ID
19930086449
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Morris, Garland J
Kennedy, Robert M
Silsby, Norman S
Date Acquired
August 16, 2013
Publication Date
November 27, 1950
Report/Patent Number
NACA-RM-L50I28
Accession Number
93R15739
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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