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Experimental investigation of the aerodynamic characteristics of an air-to-air missile employing cruciform wings and tail of rectangular plan form at Mach numbers of 1.4 and 1.9
Document ID
19930087422
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mead, Merrill H
Date Acquired
August 16, 2013
Publication Date
February 16, 1953
Report/Patent Number
NACA-RM-A52K14
Report Number: NACA-RM-A52K14
Accession Number
93R16712
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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