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An investigation of the transonic area rule by flight tests of a sweptback wing on a cylindrical body with and without body indentation between Mach numbers 0.9 and 1.8
Document ID
19930087956
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hoffman, Sherwood
Date Acquired
August 29, 2013
Publication Date
December 8, 1953
Report/Patent Number
NACA-RM-L53J20a
Report Number: NACA-RM-L53J20a
Accession Number
93R17246
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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