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Longitudinal Stability, Control Effectiveness, and Drag Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Configuration Having an Unswept Tapered Wing of Aspect Ratio 3.0 and NACA 65A004.5 Airfoil Sections
Document ID
19930087467
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mcfall, John C , Jr
Hollinger, James A
Date Acquired
August 16, 2013
Publication Date
January 20, 1953
Report/Patent Number
NACA-RM-L52L04
Report Number: NACA-RM-L52L04
Accession Number
93R16757
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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