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Low-speed Investigation of the Effects of Nacelles on the Longitudinal Aerodynamic Characteristics of a 60 Degree Sweptback Delta-wing - Fuselage Combination with NACA 65A003 Airfoil Sections
Document ID
19930087098
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Scallion, William I
Date Acquired
August 16, 2013
Publication Date
July 23, 1952
Report/Patent Number
NACA-RM-L52F04
Report Number: NACA-RM-L52F04
Accession Number
93R16388
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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