The stability conditions of Ente (duck) airplanes are investigated in this report. In developing the formulas, which afford an approximate solution, the unimportant effect of the height of the C.G. and the moment of the residual resistance are neglected. The effect of downwash from the forward horizontal empennage on the wing are also disregarded.
Static longitudinal stability of "Ente" airplanes
1931-03-01
Sonstige
Keine Angabe
Englisch
Static longitudinal stability of "Ente" airplanes
TIBKAT | 1931
|Static longitudinal stability of "Ente" airplanes
Engineering Index Backfile | 1930
|Equalization of moments and static longitudinal stability of airplanes
Engineering Index Backfile | 1929
|Longitudinal stability of airplanes
Engineering Index Backfile | 1923
|Equalization of moments and static longitudinal stability of airplanes
Engineering Index Backfile | 1929
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