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Longitudinal-control Effectiveness and Downwash Characteristics at a Mach Number of 1.24 of a 1/30-scale Semispan Model of the Bell X-5 Airplane as Determined by the NACA Wing-flow Method
Document ID
19930086544
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sawyer, Richard H
Kennedy, Robert M
Morris, Garland J
Date Acquired
August 16, 2013
Publication Date
January 8, 1951
Report/Patent Number
NACA-RM-L50K15
Report Number: NACA-RM-L50K15
Accession Number
93R15834
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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