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Aerodynamic Characteristics at a Mach Number of 4.06 of a Typical Supersonic Airplane Model Using Body and Vertical-tail Wedges to Improve Directional Stability
Document ID
19930089807
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Dunning, Robert W
Date Acquired
August 16, 2013
Publication Date
December 3, 1957
Report/Patent Number
NACA-RM-L57I10
Report Number: NACA-RM-L57I10
Accession Number
93R19097
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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