NASA NTRS · 19930094664
Stipa Monoplane with Venturi Fuselage
Abstract
This 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.
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Luigi Stipa. 1934-09-01. Stipa Monoplane with Venturi Fuselage. https://ntrs.nasa.gov/citations/19930094664
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