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    Stipa Monoplane with Venturi Fuselage (1934)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: 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.
    Type: NACA-TM-753
    Format: application/pdf
    Location Call Number Expected Availability
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