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.
Stipa Monoplane with Venturi Fuselage
1934-09-01
Sonstige
Keine Angabe
Englisch
Stipa Monoplane with Venturi Fuselage
Engineering Index Backfile | 1934
|Emerald Group Publishing | 1933
|Stipa-Caproni tubular monoplane
Engineering Index Backfile | 1933
|Stipa-Caproni tubular monoplane
Engineering Index Backfile | 1933
|Stipa-Caproni tubular monoplane
Engineering Index Backfile | 1933
|