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Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effectiveness at Supersonic Speeds of a 30-percent Chord, 50-percent Semispan Elevon as a Lateral Control Device
Document ID
19930086476
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Olson, Robert N
Mead, Merrill H
Date Acquired
August 16, 2013
Publication Date
January 18, 1951
Report/Patent Number
NACA-RM-A50K07
Report Number: NACA-RM-A50K07
Accession Number
93R15766
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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