A nomogram is developed which renders it possible by drawing a few lines, to determine: the location of the center of gravity for zero wing and tail moments; the longitudinal dihedral angle; the tail coefficient F(sub h) iota/F(sub t). Moreover there is no difficulty in determining the magnitude of the restoring moment or of the unstable moment.
The balance of moments and the static longitudinal stability of airplanes
1929-12-01
Miscellaneous
No indication
English
Equalization of moments and static longitudinal stability of airplanes
Engineering Index Backfile | 1929
|Static longitudinal stability of "Ente" airplanes
NTRS | 1931
|Static longitudinal stability of "Ente" airplanes
TIBKAT | 1931
|Static longitudinal stability of "Ente" airplanes
Engineering Index Backfile | 1930
|