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The Effects of an Inverse-taper Leading-edge Flap on the Aerodynamic Characteristics in Pitch of a Wing-body Combination Having an Aspect Ratio of 3 to 45 Degrees of Sweepback at Mach Numbers to 0.92
Document ID
19930085266
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Demele, Fred A
POWELL K HARMON
Date Acquired
August 16, 2013
Publication Date
August 1, 1958
Report/Patent Number
NACA-TN-4366
Accession Number
93R14556
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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