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Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness of an inboard elevon as a longitudinal- and lateral-control device at subsonic and supersonic speeds
Document ID
19930086895
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Pfyl, Frank A
Date Acquired
August 29, 2013
Publication Date
December 4, 1951
Report/Patent Number
NACA-RM-A51I18
Accession Number
93R16185
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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