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Experimental Investigation at Low Speed of the Effects of Wing Position on the Static Stability of Models Having Fuselages of Various Cross Section and Unswept and 45 Degrees Sweptback Surfaces
Document ID
19930084643
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Letko, William
Date Acquired
August 16, 2013
Publication Date
November 1, 1956
Report/Patent Number
NACA-TN-3857
Report Number: NACA-TN-3857
Accession Number
93R13933
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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