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Stipa Monoplane with Venturi FuselageThis report presents a detailed examination of the factors that went into the design of the Stipa monoplane. The model tested in the wind tunnel was made dissymmetrical externally, in order to produce a lift even at an angle of attack of 0 degrees with respect to the longitudinal axis of the tube.
Document ID
19930094664
Document Type
Other
Authors
Stipa, Luigi
Date Acquired
September 6, 2013
Publication Date
September 1, 1934
Report/Patent Number
NACA-TM-753
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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