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Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effectiveness of an Elevon as a Longitudinal Control and the Effects of Camber and Twist on the Maximum Lift-drag Ratio at Supersonic Speeds
Document ID
19930086313
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Olson, Robert N
Mead, Merrill H
Date Acquired
August 16, 2013
Publication Date
May 8, 1950
Report/Patent Number
NACA-RM-A50A31a
Report Number: NACA-RM-A50A31a
Accession Number
93R15603
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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