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Effects of a Leading-edge Slat and a Trailing-edge Split Flap on the Aerodynamic Characteristics of a Wing-fuselage Combination Having a Nearly Triangular Wing of Aspect Ratio 2.9 at Mach Numbers from 0.60 to 0.92
Document ID
19930090339
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Demele, Fred A
Date Acquired
August 15, 2013
Publication Date
January 12, 1958
Report/Patent Number
NACA-RM-A57H19
Report Number: NACA-RM-A57H19
Accession Number
93R19629
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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