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A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degree Sweptback-wing-body Combination
Document ID
19930087423
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Robinson, Harold L
Date Acquired
August 16, 2013
Publication Date
February 9, 1953
Report/Patent Number
NACA-RM-L52L12
Report Number: NACA-RM-L52L12
Accession Number
93R16713
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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