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An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback : Force Characteristics of the Complete Configuration and Its Various Components at Mach Numbers of 1.40 and 1.59
Document ID
19930086531
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Smith, Norman F
Marte, Jack E
Date Acquired
August 16, 2013
Publication Date
January 22, 1951
Report/Patent Number
NACA-RM-L50K14
Accession Number
93R15821
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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