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A flight investigation of the transonic area rule for a 52.5 degree sweptback wing-body configuration at Mach numbers between 0.8 and 1.6
Document ID
19930088324
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hoffman, Sherwood
Date Acquired
August 29, 2013
Publication Date
November 19, 1954
Report/Patent Number
NACA-RM-L54H13a
Report Number: NACA-RM-L54H13a
Accession Number
93R17614
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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