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Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Subsonic Mach and Reynolds Number Effects on the Characteristics of the Wing and on the Effectiveness of an Elevon
Document ID
19930085437
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Reynolds, Robert M
Smith, Donald W
Date Acquired
August 16, 2013
Publication Date
October 11, 1948
Report/Patent Number
NACA-RM-A8D20
Report Number: NACA-RM-A8D20
Accession Number
93R14727
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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