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Static longitudinal stability of "Ente" airplanesThe stability conditions of Ente (duck) airplanes are investigated in this report. In developing the formulas, which afford an approximate solution, the unimportant effect of the height of the C.G. and the moment of the residual resistance are neglected. The effect of downwash from the forward horizontal empennage on the wing are also disregarded.
Document ID
19930094804
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kiel, Heinrich Georg
Date Acquired
September 6, 2013
Publication Date
March 1, 1931
Report/Patent Number
NACA-TM-612
Report Number: NACA-TM-612
Accession Number
93R23724
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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