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Longitudinal Characteristics at Mach Number of 1.24 of 1/30-scale Semispan Model of Bell X-5 Variable-sweep Airplane with Wing Swept Back 60 Degrees : from Tests by NACA Wing-flow Method
Document ID
19930086179
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Silsby, Norman S
Morris, Garland J
Kennedy, Robert M
Date Acquired
August 16, 2013
Publication Date
October 12, 1950
Report/Patent Number
NACA-RM-L50E02a
Report Number: NACA-RM-L50E02a
Accession Number
93R15469
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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