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Effects of a fuselage flap dive brake on the aerodynamic characteristics of 1/30 scale semispan model of the Bell X-5 variable-sweep airplane at a Mach number 1.24 as determined by the NACA wing flow method
Document ID
19930086470
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kennedy, Robert M
Date Acquired
August 29, 2013
Publication Date
February 8, 1951
Report/Patent Number
NACA-RM-L50L11a
Report Number: NACA-RM-L50L11a
Accession Number
93R15760
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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