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Langley 9-inch Supersonic Tunnel Tests of Several Modifications of a Supersonic Missile Having Tandem Cruciform Lifting Surfaces : Three-component Data Results of Models Having Ratios of Wing Span to Tail Span Equal to and Less than 1 and Some Static
Document ID
19930086355
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Rainey, Robert W
Date Acquired
August 16, 2013
Publication Date
March 7, 1951
Report/Patent Number
NACA-RM-L50G07
Report Number: NACA-RM-L50G07
Accession Number
93R15645
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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