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Effects of Leading-edge Chord Extensions and an All-movable Horizontal Tail on the Aerodynamic Characteristics of a Wing-body Combination Employing a Triangular Wing of Aspect Ratio 3 Mounted in a High Position at Subsonic and Supersonic Speeds
Document ID
19930088269
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wetzel, Benton E
Pfyl, Frank A
Date Acquired
August 16, 2013
Publication Date
January 6, 1954
Report/Patent Number
NACA-RM-A53J14a
Report Number: NACA-RM-A53J14a
Accession Number
93R17559
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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