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Influence of Fuselage and Canard-type Control Surface on the Flow Field Adjacent to a Rearward Fuselage Station at a Mach Number of 2.0 : Data Presentation
Document ID
19930087136
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Obery, Leonard J
Fradenburgh, Evan A
Mello, John F
Date Acquired
August 16, 2013
Publication Date
January 21, 1952
Report/Patent Number
NACA-RM-E51K05
Report Number: NACA-RM-E51K05
Accession Number
93R16426
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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