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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
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Luigi Stipa (Rivista Aeronautica)
Date Acquired
September 6, 2013
Publication Date
September 1, 1934
Subject Category
Aircraft Design, Testing and Performance
Report/Patent Number
NACA-TM-753
Report Number: NACA-TM-753
Accession Number
93R23584
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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